Explore: Subsonic Flow

Discover books, insights, and more — all in one place.

Learn more about Subsonic Flow with top reads curated from trusted sources — all in one place.

Topic Search

Search for any topic

AI-Generated Overview About “subsonic-flow”:


Books Results

Source: The Open Library

The Open Library Search Results

Search results from The Open Library

1The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel

By

“The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel” Metadata:

  • Title: ➤  The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel
  • Author:
  • Language: English
  • Number of Pages: Median: 186
  • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor - Available from the National Technical Information Service
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Springfield, VA - Moffett Field, Calif

“The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1998
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

Online Access

Downloads Are Not Available:

The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

Online Borrowing:

    Online Marketplaces

    Find The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel at online marketplaces:


    2Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code

    By

    “Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code” Metadata:

    • Title: ➤  Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
    • Author:
    • Language: English
    • Number of Pages: Median: 77
    • Publisher: ➤  Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  Hampton, Va - Springfield, VA - [Springfield, Va

    “Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1996
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

    Online Borrowing:

      Online Marketplaces

      Find Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code at online marketplaces:


      3Implementation of a two-equation K-[omega] turbulence model in NPARC

      By

      “Implementation of a two-equation K-[omega] turbulence model in NPARC” Metadata:

      • Title: ➤  Implementation of a two-equation K-[omega] turbulence model in NPARC
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - [Washington, DC]

      “Implementation of a two-equation K-[omega] turbulence model in NPARC” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1996
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

      Online Borrowing:

        Online Marketplaces

        Find Implementation of a two-equation K-[omega] turbulence model in NPARC at online marketplaces:


        4Higher-order approximations in interactive airfoil calculations

        By

        “Higher-order approximations in interactive airfoil calculations” Metadata:

        • Title: ➤  Higher-order approximations in interactive airfoil calculations
        • Author:
        • Language: English
        • Number of Pages: Median: 102
        • Publisher: ➤  University of Toronto - Institute for Aerospace Studies
        • Publish Date:
        • Publish Location: [Downsview, Ont.]

        “Higher-order approximations in interactive airfoil calculations” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1987
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Marketplaces

        Find Higher-order approximations in interactive airfoil calculations at online marketplaces:


        5Analysis of boundary conditions for SSME subsonic internal viscous flow analysis

        By

        “Analysis of boundary conditions for SSME subsonic internal viscous flow analysis” Metadata:

        • Title: ➤  Analysis of boundary conditions for SSME subsonic internal viscous flow analysis
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - Computational Mechanics Corporation
        • Publish Date:
        • Publish Location: ➤  Knoxville, TN - [Washington, DC - Springfield, Va

        “Analysis of boundary conditions for SSME subsonic internal viscous flow analysis” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1986
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

        Online Borrowing:

          Online Marketplaces

          Find Analysis of boundary conditions for SSME subsonic internal viscous flow analysis at online marketplaces:


          6STARS

          By

          “STARS” Metadata:

          • Title: STARS
          • Author:
          • Language: English
          • Number of Pages: Median: 160
          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - Edwards, Calif

          “STARS” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1990
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Access

          Downloads Are Not Available:

          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

          Online Borrowing:

            Online Marketplaces

            Find STARS at online marketplaces:


            7An extended Lagrangian method

            By

            “An extended Lagrangian method” Metadata:

            • Title: An extended Lagrangian method
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  Springfield, Va - [Washington, D.C - [Washington, DC

            “An extended Lagrangian method” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1992
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

            Downloads Are Not Available:

            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

            Online Borrowing:

              Online Marketplaces

              Find An extended Lagrangian method at online marketplaces:


              8A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept

              By

              “A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept” Metadata:

              • Title: ➤  A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: Hampton, Va - [Springfield, Va

              “A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1995
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

              Online Borrowing:

                Online Marketplaces

                Find A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept at online marketplaces:


                9Description of panel method code ANTARES

                By

                “Description of panel method code ANTARES” Metadata:

                • Title: ➤  Description of panel method code ANTARES
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - Available from NASA Center for Aerospace Information
                • Publish Date:
                • Publish Location: ➤  Moffett, Field, Calif - Hanover, MD

                “Description of panel method code ANTARES” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 2000
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Access

                Downloads Are Not Available:

                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                Online Borrowing:

                  Online Marketplaces

                  Find Description of panel method code ANTARES at online marketplaces:


                  10An extended Lagrangian method

                  By

                  “An extended Lagrangian method” Metadata:

                  • Title: An extended Lagrangian method
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                  • Publish Date:
                  • Publish Location: ➤  Springfield, Va - [Washington, D.C - [Washington, DC

                  “An extended Lagrangian method” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1992
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

                  Online Access

                  Downloads Are Not Available:

                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                  Online Borrowing:

                    Online Marketplaces

                    Find An extended Lagrangian method at online marketplaces:


                    11Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D

                    By

                    “Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D” Metadata:

                    • Title: ➤  Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                    • Publish Date:
                    • Publish Location: Hampton, Va - [Springfield, Va

                    “Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1996
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

                    Online Access

                    Downloads Are Not Available:

                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                    Online Borrowing:

                      Online Marketplaces

                      Find Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D at online marketplaces:


                      12Wing pressure distributions from subsonic tests of a high-wing transport model

                      By

                      “Wing pressure distributions from subsonic tests of a high-wing transport model” Metadata:

                      • Title: ➤  Wing pressure distributions from subsonic tests of a high-wing transport model
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                      • Publish Date:
                      • Publish Location: Hampton, Va - [Springfield, Va

                      “Wing pressure distributions from subsonic tests of a high-wing transport model” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1995
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

                      Online Access

                      Downloads Are Not Available:

                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                      Online Borrowing:

                        Online Marketplaces

                        Find Wing pressure distributions from subsonic tests of a high-wing transport model at online marketplaces:


                        13Doppler global velocimetry at NASA Glenn Research Center

                        By

                        “Doppler global velocimetry at NASA Glenn Research Center” Metadata:

                        • Title: ➤  Doppler global velocimetry at NASA Glenn Research Center
                        • Author:
                        • Language: English
                        • Publisher: ➤  Available from NASA Center for Aerospace Information - National Technical Information Service [distributor - National Aeronautics and Space Administration, Glenn Research Center
                        • Publish Date:
                        • Publish Location: ➤  [Cleveland, Ohio] - Springfield, VA - Hanover, MD

                        “Doppler global velocimetry at NASA Glenn Research Center” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 2003
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

                        Online Access

                        Downloads Are Not Available:

                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                        Online Borrowing:

                          Online Marketplaces

                          Find Doppler global velocimetry at NASA Glenn Research Center at online marketplaces:


                          14High frequency flow/structural interaction in dense subsonic fluids

                          By

                          “High frequency flow/structural interaction in dense subsonic fluids” Metadata:

                          • Title: ➤  High frequency flow/structural interaction in dense subsonic fluids
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - National Aeronautics and Space Administration, Marshall Space Flight Center - Rockwell Aerospace, Space Systems Division, Huntsville Operations
                          • Publish Date:
                          • Publish Location: ➤  Marshall Space Flight Center, Ala - [Springfield, Va - Springfield, Va - [Huntsville, Ala.] - [Washington, DC

                          “High frequency flow/structural interaction in dense subsonic fluids” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1994
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

                          Online Access

                          Downloads Are Not Available:

                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                          Online Borrowing:

                            Online Marketplaces

                            Find High frequency flow/structural interaction in dense subsonic fluids at online marketplaces:


                            15Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report

                            By

                            “Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report” Metadata:

                            • Title: ➤  Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report
                            • Author:
                            • Language: English
                            • Publisher: ➤  Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
                            • Publish Date:
                            • Publish Location: ➤  [Cleveland, Ohio] - Hanover, MD

                            “Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 2001
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

                            Online Access

                            Downloads Are Not Available:

                            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                            Online Borrowing:

                              Online Marketplaces

                              Find Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report at online marketplaces:


                              16Analytical studies of boundary layer generated aircraft interior noise

                              By

                              “Analytical studies of boundary layer generated aircraft interior noise” Metadata:

                              • Title: ➤  Analytical studies of boundary layer generated aircraft interior noise
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - Boston University, College of Engineering
                              • Publish Date:
                              • Publish Location: ➤  Boston, MA - [Washington, DC - Springfield, Va

                              “Analytical studies of boundary layer generated aircraft interior noise” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1997
                              • Is Full Text Available: No
                              • Is The Book Public: No
                              • Access Status: No_ebook

                              Online Access

                              Downloads Are Not Available:

                              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                              Online Borrowing:

                                Online Marketplaces

                                Find Analytical studies of boundary layer generated aircraft interior noise at online marketplaces:


                                17Advanced method for computing the flow around wings with rear separation and ground effect

                                By

                                “Advanced method for computing the flow around wings with rear separation and ground effect” Metadata:

                                • Title: ➤  Advanced method for computing the flow around wings with rear separation and ground effect
                                • Author:
                                • Number of Pages: Median: 62
                                • Publisher: ➤  DFVLR Institut fur Theoretische Stromungsmechanik
                                • Publish Date:
                                • Publish Location: Gottingen

                                “Advanced method for computing the flow around wings with rear separation and ground effect” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1986
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

                                Online Marketplaces

                                Find Advanced method for computing the flow around wings with rear separation and ground effect at online marketplaces:


                                18External boundary conditions for three-dimensional problems of computational aerodynamics

                                By

                                “External boundary conditions for three-dimensional problems of computational aerodynamics” Metadata:

                                • Title: ➤  External boundary conditions for three-dimensional problems of computational aerodynamics
                                • Author:
                                • Language: English
                                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                • Publish Date:
                                • Publish Location: Hampton, Va - [Springfield, Va

                                “External boundary conditions for three-dimensional problems of computational aerodynamics” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1997
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

                                Online Access

                                Downloads Are Not Available:

                                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                Online Borrowing:

                                  Online Marketplaces

                                  Find External boundary conditions for three-dimensional problems of computational aerodynamics at online marketplaces:


                                  19Prediction of vortex shedding from circular and noncircular bodies in subsonic flow

                                  By

                                  “Prediction of vortex shedding from circular and noncircular bodies in subsonic flow” Metadata:

                                  • Title: ➤  Prediction of vortex shedding from circular and noncircular bodies in subsonic flow
                                  • Author:
                                  • Number of Pages: Median: 163
                                  • Publisher: Langley Research Center
                                  • Publish Date:
                                  • Publish Location: Hampton, Va

                                  “Prediction of vortex shedding from circular and noncircular bodies in subsonic flow” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 1987
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

                                  Online Marketplaces

                                  Find Prediction of vortex shedding from circular and noncircular bodies in subsonic flow at online marketplaces:


                                  20Shear flow control of cold and heated rectangular jets by mechanical tabs

                                  By

                                  “Shear flow control of cold and heated rectangular jets by mechanical tabs” Metadata:

                                  • Title: ➤  Shear flow control of cold and heated rectangular jets by mechanical tabs
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                  • Publish Date:
                                  • Publish Location: ➤  [Washington, DC - Springfield, Va

                                  “Shear flow control of cold and heated rectangular jets by mechanical tabs” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 1989
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

                                  Online Access

                                  Downloads Are Not Available:

                                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                  Online Borrowing:

                                    Online Marketplaces

                                    Find Shear flow control of cold and heated rectangular jets by mechanical tabs at online marketplaces:


                                    21Correction for wall-interference by means of a measured-boundary-conditon method

                                    By

                                    “Correction for wall-interference by means of a measured-boundary-conditon method” Metadata:

                                    • Title: ➤  Correction for wall-interference by means of a measured-boundary-conditon method
                                    • Author:
                                    • Number of Pages: Median: 41
                                    • Publisher: National Aerospace Laboratory
                                    • Publish Date:
                                    • Publish Location: Amsterdam

                                    “Correction for wall-interference by means of a measured-boundary-conditon method” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

                                    • First Year Published: 1984
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
                                    • Access Status: No_ebook

                                    Online Marketplaces

                                    Find Correction for wall-interference by means of a measured-boundary-conditon method at online marketplaces:


                                    22Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet

                                    By

                                    “Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Metadata:

                                    • Title: ➤  Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                    • Publish Date:
                                    • Publish Location: Hampton, Va - [Springfield, Va

                                    “Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

                                    • First Year Published: 1999
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
                                    • Access Status: No_ebook

                                    Online Access

                                    Downloads Are Not Available:

                                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                    Online Borrowing:

                                      Online Marketplaces

                                      Find Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet at online marketplaces:


                                      23Investigation of parabolic computational techniques for internal high-speed viscous flows

                                      By

                                      “Investigation of parabolic computational techniques for internal high-speed viscous flows” Metadata:

                                      • Title: ➤  Investigation of parabolic computational techniques for internal high-speed viscous flows
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - United Technologies Research Center
                                      • Publish Date:
                                      • Publish Location: ➤  East Hartford, CT - Hampton, Va

                                      “Investigation of parabolic computational techniques for internal high-speed viscous flows” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

                                      • First Year Published: 1985
                                      • Is Full Text Available: No
                                      • Is The Book Public: No
                                      • Access Status: No_ebook

                                      Online Access

                                      Downloads Are Not Available:

                                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                      Online Borrowing:

                                        Online Marketplaces

                                        Find Investigation of parabolic computational techniques for internal high-speed viscous flows at online marketplaces:


                                        24Application of chimera grid scheme to combustor flowfields at all speeds

                                        By

                                        “Application of chimera grid scheme to combustor flowfields at all speeds” Metadata:

                                        • Title: ➤  Application of chimera grid scheme to combustor flowfields at all speeds
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion - National Technical Information Service, distributor
                                        • Publish Date:
                                        • Publish Location: ➤  [Cleveland, Ohio] - [Springfield, Va

                                        “Application of chimera grid scheme to combustor flowfields at all speeds” Subjects and Themes:

                                        Edition Identifiers:

                                        Access and General Info:

                                        • First Year Published: 1997
                                        • Is Full Text Available: No
                                        • Is The Book Public: No
                                        • Access Status: No_ebook

                                        Online Access

                                        Downloads Are Not Available:

                                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                        Online Borrowing:

                                          Online Marketplaces

                                          Find Application of chimera grid scheme to combustor flowfields at all speeds at online marketplaces:


                                          25Response of high subsonic jet to nonaxisymmetric disturbances

                                          By

                                          “Response of high subsonic jet to nonaxisymmetric disturbances” Metadata:

                                          • Title: ➤  Response of high subsonic jet to nonaxisymmetric disturbances
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor - National Aeronautics and Space Administration
                                          • Publish Date:
                                          • Publish Location: ➤  Springfield, Va - Reston, VA - [Washington, DC

                                          “Response of high subsonic jet to nonaxisymmetric disturbances” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1997
                                          • Is Full Text Available: No
                                          • Is The Book Public: No
                                          • Access Status: No_ebook

                                          Online Access

                                          Downloads Are Not Available:

                                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                          Online Borrowing:

                                            Online Marketplaces

                                            Find Response of high subsonic jet to nonaxisymmetric disturbances at online marketplaces:


                                            26Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators

                                            By

                                            “Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators” Metadata:

                                            • Title: ➤  Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                            • Publish Date:
                                            • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                            “Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators” Subjects and Themes:

                                            Edition Identifiers:

                                            Access and General Info:

                                            • First Year Published: 1994
                                            • Is Full Text Available: No
                                            • Is The Book Public: No
                                            • Access Status: No_ebook

                                            Online Access

                                            Downloads Are Not Available:

                                            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                            Online Borrowing:

                                              Online Marketplaces

                                              Find Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators at online marketplaces:


                                              27A numerical simulator for three-dimensional flows through vibrating blade rows

                                              By

                                              “A numerical simulator for three-dimensional flows through vibrating blade rows” Metadata:

                                              • Title: ➤  A numerical simulator for three-dimensional flows through vibrating blade rows
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
                                              • Publish Date:
                                              • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

                                              “A numerical simulator for three-dimensional flows through vibrating blade rows” Subjects and Themes:

                                              Edition Identifiers:

                                              Access and General Info:

                                              • First Year Published: 1998
                                              • Is Full Text Available: No
                                              • Is The Book Public: No
                                              • Access Status: No_ebook

                                              Online Access

                                              Downloads Are Not Available:

                                              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                              Online Borrowing:

                                                Online Marketplaces

                                                Find A numerical simulator for three-dimensional flows through vibrating blade rows at online marketplaces:


                                                28Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle

                                                By

                                                “Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle” Metadata:

                                                • Title: ➤  Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
                                                • Author:
                                                • Language: English
                                                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                                • Publish Date:
                                                • Publish Location: Hampton, Va - [Springfield, Va

                                                “Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle” Subjects and Themes:

                                                Edition Identifiers:

                                                Access and General Info:

                                                • First Year Published: 1996
                                                • Is Full Text Available: No
                                                • Is The Book Public: No
                                                • Access Status: No_ebook

                                                Online Access

                                                Downloads Are Not Available:

                                                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                Online Borrowing:

                                                  Online Marketplaces

                                                  Find Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle at online marketplaces:


                                                  29Role of boundary conditions in Monte Carlo simulation of MEMS devices

                                                  By

                                                  “Role of boundary conditions in Monte Carlo simulation of MEMS devices” Metadata:

                                                  • Title: ➤  Role of boundary conditions in Monte Carlo simulation of MEMS devices
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
                                                  • Publish Date:
                                                  • Publish Location: ➤  Washington, D.C - Springfield, Va

                                                  “Role of boundary conditions in Monte Carlo simulation of MEMS devices” Subjects and Themes:

                                                  Edition Identifiers:

                                                  Access and General Info:

                                                  • First Year Published: 1997
                                                  • Is Full Text Available: No
                                                  • Is The Book Public: No
                                                  • Access Status: No_ebook

                                                  Online Access

                                                  Downloads Are Not Available:

                                                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                  Online Borrowing:

                                                    Online Marketplaces

                                                    Find Role of boundary conditions in Monte Carlo simulation of MEMS devices at online marketplaces:


                                                    30Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds

                                                    By

                                                    “Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” Metadata:

                                                    • Title: ➤  Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
                                                    • Author:
                                                    • Language: English
                                                    • Number of Pages: Median: 51
                                                    • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                                                    • Publish Date:
                                                    • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                                    “Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1991
                                                    • Is Full Text Available: No
                                                    • Is The Book Public: No
                                                    • Access Status: No_ebook

                                                    Online Access

                                                    Downloads Are Not Available:

                                                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                    Online Borrowing:

                                                      Online Marketplaces

                                                      Find Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds at online marketplaces:


                                                      31Computational investigations of noise suppression in subsonic round jets

                                                      By

                                                      “Computational investigations of noise suppression in subsonic round jets” Metadata:

                                                      • Title: ➤  Computational investigations of noise suppression in subsonic round jets
                                                      • Author:
                                                      • Language: English
                                                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                      • Publish Date:
                                                      • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                      “Computational investigations of noise suppression in subsonic round jets” Subjects and Themes:

                                                      Edition Identifiers:

                                                      Access and General Info:

                                                      • First Year Published: 1997
                                                      • Is Full Text Available: No
                                                      • Is The Book Public: No
                                                      • Access Status: No_ebook

                                                      Online Access

                                                      Downloads Are Not Available:

                                                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                      Online Borrowing:

                                                        Online Marketplaces

                                                        Find Computational investigations of noise suppression in subsonic round jets at online marketplaces:


                                                        32RNS applications for interacting sub- and supersonic flows

                                                        By

                                                        “RNS applications for interacting sub- and supersonic flows” Metadata:

                                                        • Title: ➤  RNS applications for interacting sub- and supersonic flows
                                                        • Author:
                                                        • Language: English
                                                        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                        • Publish Date:
                                                        • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                        “RNS applications for interacting sub- and supersonic flows” Subjects and Themes:

                                                        Edition Identifiers:

                                                        Access and General Info:

                                                        • First Year Published: 1997
                                                        • Is Full Text Available: No
                                                        • Is The Book Public: No
                                                        • Access Status: No_ebook

                                                        Online Access

                                                        Downloads Are Not Available:

                                                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                        Online Borrowing:

                                                          Online Marketplaces

                                                          Find RNS applications for interacting sub- and supersonic flows at online marketplaces:


                                                          33Entry dispersion analysis for the Stardust comet sample return capsule

                                                          By

                                                          “Entry dispersion analysis for the Stardust comet sample return capsule” Metadata:

                                                          • Title: ➤  Entry dispersion analysis for the Stardust comet sample return capsule
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
                                                          • Publish Date:
                                                          • Publish Location: ➤  Reston, VA - Springfield, Va - [Washington, D.C

                                                          “Entry dispersion analysis for the Stardust comet sample return capsule” Subjects and Themes:

                                                          Edition Identifiers:

                                                          Access and General Info:

                                                          • First Year Published: 1997
                                                          • Is Full Text Available: No
                                                          • Is The Book Public: No
                                                          • Access Status: No_ebook

                                                          Online Access

                                                          Downloads Are Not Available:

                                                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                          Online Borrowing:

                                                            Online Marketplaces

                                                            Find Entry dispersion analysis for the Stardust comet sample return capsule at online marketplaces:


                                                            34Measurement of gust response on a turbine cascade

                                                            By

                                                            “Measurement of gust response on a turbine cascade” Metadata:

                                                            • Title: ➤  Measurement of gust response on a turbine cascade
                                                            • Author:
                                                            • Language: English
                                                            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                            • Publish Date:
                                                            • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                                            “Measurement of gust response on a turbine cascade” Subjects and Themes:

                                                            Edition Identifiers:

                                                            Access and General Info:

                                                            • First Year Published: 1995
                                                            • Is Full Text Available: No
                                                            • Is The Book Public: No
                                                            • Access Status: No_ebook

                                                            Online Access

                                                            Downloads Are Not Available:

                                                            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                            Online Borrowing:

                                                              Online Marketplaces

                                                              Find Measurement of gust response on a turbine cascade at online marketplaces:


                                                              35Natural rolling responses of a delta wing in transonic and subsonic flows

                                                              By

                                                              “Natural rolling responses of a delta wing in transonic and subsonic flows” Metadata:

                                                              • Title: ➤  Natural rolling responses of a delta wing in transonic and subsonic flows
                                                              • Author:
                                                              • Language: English
                                                              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Aeronautics
                                                              • Publish Date:
                                                              • Publish Location: ➤  [Washington, DC - Reston, Va - [Springfield, Va

                                                              “Natural rolling responses of a delta wing in transonic and subsonic flows” Subjects and Themes:

                                                              Edition Identifiers:

                                                              Access and General Info:

                                                              • First Year Published: 1996
                                                              • Is Full Text Available: No
                                                              • Is The Book Public: No
                                                              • Access Status: No_ebook

                                                              Online Access

                                                              Downloads Are Not Available:

                                                              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                              Online Borrowing:

                                                                Online Marketplaces

                                                                Find Natural rolling responses of a delta wing in transonic and subsonic flows at online marketplaces:


                                                                36Feasibility study of a single component scanning laser doppler anemometer

                                                                By

                                                                “Feasibility study of a single component scanning laser doppler anemometer” Metadata:

                                                                • Title: ➤  Feasibility study of a single component scanning laser doppler anemometer
                                                                • Author:
                                                                • Number of Pages: Median: 46
                                                                • Publisher: ➤  Dept. of Aerospace Science and Engineering
                                                                • Publish Date:
                                                                • Publish Location: [Downsview, Ont.]

                                                                “Feasibility study of a single component scanning laser doppler anemometer” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1978
                                                                • Is Full Text Available: No
                                                                • Is The Book Public: No
                                                                • Access Status: No_ebook

                                                                Online Marketplaces

                                                                Find Feasibility study of a single component scanning laser doppler anemometer at online marketplaces:


                                                                37Pressure distribution and reattachment length of subsonic flow over a rearward-facing step

                                                                By

                                                                “Pressure distribution and reattachment length of subsonic flow over a rearward-facing step” Metadata:

                                                                • Title: ➤  Pressure distribution and reattachment length of subsonic flow over a rearward-facing step
                                                                • Author:
                                                                • Number of Pages: Median: 69
                                                                • Publisher: ➤  Dept. of Aerospace Science and Engineering
                                                                • Publish Date:
                                                                • Publish Location: [Downsview, Ont.]

                                                                “Pressure distribution and reattachment length of subsonic flow over a rearward-facing step” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1979
                                                                • Is Full Text Available: No
                                                                • Is The Book Public: No
                                                                • Access Status: No_ebook

                                                                Online Marketplaces

                                                                Find Pressure distribution and reattachment length of subsonic flow over a rearward-facing step at online marketplaces:


                                                                38Application of linearized transonic theory to tunnel blockage interference

                                                                By

                                                                “Application of linearized transonic theory to tunnel blockage interference” Metadata:

                                                                • Title: ➤  Application of linearized transonic theory to tunnel blockage interference
                                                                • Author:
                                                                • Number of Pages: Median: 28
                                                                • Publisher: ➤  Arnold Engineering Development Center
                                                                • Publish Date:
                                                                • Publish Location: Arnold AF Station, Tenn

                                                                “Application of linearized transonic theory to tunnel blockage interference” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1974
                                                                • Is Full Text Available: No
                                                                • Is The Book Public: No
                                                                • Access Status: No_ebook

                                                                Online Marketplaces

                                                                Find Application of linearized transonic theory to tunnel blockage interference at online marketplaces:


                                                                39Implementation of and measurement with the LIPA technique in a subsonic jet

                                                                By

                                                                “Implementation of and measurement with the LIPA technique in a subsonic jet” Metadata:

                                                                • Title: ➤  Implementation of and measurement with the LIPA technique in a subsonic jet
                                                                • Author:
                                                                • Language: English
                                                                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Michigan State University, Dept. of Mechanical Engineering
                                                                • Publish Date:
                                                                • Publish Location: ➤  Springfield, Va - [Washington, DC - East Lansing, MI

                                                                “Implementation of and measurement with the LIPA technique in a subsonic jet” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1994
                                                                • Is Full Text Available: No
                                                                • Is The Book Public: No
                                                                • Access Status: No_ebook

                                                                Online Access

                                                                Downloads Are Not Available:

                                                                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                Online Borrowing:

                                                                  Online Marketplaces

                                                                  Find Implementation of and measurement with the LIPA technique in a subsonic jet at online marketplaces:


                                                                  40Determination of the pressure drag of airfoils by integration of surface pressures

                                                                  By

                                                                  “Determination of the pressure drag of airfoils by integration of surface pressures” Metadata:

                                                                  • Title: ➤  Determination of the pressure drag of airfoils by integration of surface pressures
                                                                  • Author:
                                                                  • Language: English
                                                                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                                                                  • Publish Date:
                                                                  • Publish Location: Hampton, Va - [Springfield, Va

                                                                  “Determination of the pressure drag of airfoils by integration of surface pressures” Subjects and Themes:

                                                                  Edition Identifiers:

                                                                  Access and General Info:

                                                                  • First Year Published: 1990
                                                                  • Is Full Text Available: No
                                                                  • Is The Book Public: No
                                                                  • Access Status: No_ebook

                                                                  Online Access

                                                                  Downloads Are Not Available:

                                                                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                  Online Borrowing:

                                                                    Online Marketplaces

                                                                    Find Determination of the pressure drag of airfoils by integration of surface pressures at online marketplaces:


                                                                    41A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

                                                                    By

                                                                    “A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92” Metadata:

                                                                    • Title: ➤  A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
                                                                    • Author:
                                                                    • Language: English
                                                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                                                                    • Publish Date:
                                                                    • Publish Location: Hampton, Va - [Springfield, Va

                                                                    “A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92” Subjects and Themes:

                                                                    Edition Identifiers:

                                                                    Access and General Info:

                                                                    • First Year Published: 1996
                                                                    • Is Full Text Available: No
                                                                    • Is The Book Public: No
                                                                    • Access Status: No_ebook

                                                                    Online Access

                                                                    Downloads Are Not Available:

                                                                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                    Online Borrowing:

                                                                      Online Marketplaces

                                                                      Find A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 at online marketplaces:


                                                                      42Methods of linearization in compressible flow

                                                                      By

                                                                      “Methods of linearization in compressible flow” Metadata:

                                                                      • Title: ➤  Methods of linearization in compressible flow
                                                                      • Author:
                                                                      • Number of Pages: Median: 141
                                                                      • Publisher: ➤  Wright-Patterson Air Force Base
                                                                      • Publish Date:
                                                                      • Publish Location: Dayton, Ohio

                                                                      “Methods of linearization in compressible flow” Subjects and Themes:

                                                                      Edition Identifiers:

                                                                      Access and General Info:

                                                                      • First Year Published: 1949
                                                                      • Is Full Text Available: No
                                                                      • Is The Book Public: No
                                                                      • Access Status: No_ebook

                                                                      Online Marketplaces

                                                                      Find Methods of linearization in compressible flow at online marketplaces:


                                                                      43Validation of WIND for a series of inlet flows

                                                                      By

                                                                      “Validation of WIND for a series of inlet flows” Metadata:

                                                                      • Title: ➤  Validation of WIND for a series of inlet flows
                                                                      • Author:
                                                                      • Language: English
                                                                      • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
                                                                      • Publish Date:
                                                                      • Publish Location: ➤  [Cleveland, Ohio] - Hanover, MD

                                                                      “Validation of WIND for a series of inlet flows” Subjects and Themes:

                                                                      Edition Identifiers:

                                                                      Access and General Info:

                                                                      • First Year Published: 2002
                                                                      • Is Full Text Available: No
                                                                      • Is The Book Public: No
                                                                      • Access Status: No_ebook

                                                                      Online Access

                                                                      Downloads Are Not Available:

                                                                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                      Online Borrowing:

                                                                        Online Marketplaces

                                                                        Find Validation of WIND for a series of inlet flows at online marketplaces:


                                                                        44Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes

                                                                        By

                                                                        “Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes” Metadata:

                                                                        • Title: ➤  Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes
                                                                        • Author:
                                                                        • Language: English
                                                                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                                                                        • Publish Date:
                                                                        • Publish Location: Hampton, Va - [Springfield, Va

                                                                        “Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes” Subjects and Themes:

                                                                        Edition Identifiers:

                                                                        Access and General Info:

                                                                        • First Year Published: 1995
                                                                        • Is Full Text Available: No
                                                                        • Is The Book Public: No
                                                                        • Access Status: No_ebook

                                                                        Online Access

                                                                        Downloads Are Not Available:

                                                                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                        Online Borrowing:

                                                                          Online Marketplaces

                                                                          Find Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes at online marketplaces:


                                                                          45Unsteady aerodynamics

                                                                          By

                                                                          “Unsteady aerodynamics” Metadata:

                                                                          • Title: Unsteady aerodynamics
                                                                          • Author:
                                                                          • Language: English
                                                                          • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
                                                                          • Publish Date:
                                                                          • Publish Location: ➤  Edwards, Calif - Springfield, VA

                                                                          “Unsteady aerodynamics” Subjects and Themes:

                                                                          Edition Identifiers:

                                                                          Access and General Info:

                                                                          • First Year Published: 1999
                                                                          • Is Full Text Available: No
                                                                          • Is The Book Public: No
                                                                          • Access Status: No_ebook

                                                                          Online Access

                                                                          Downloads Are Not Available:

                                                                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                          Online Borrowing:

                                                                            Online Marketplaces

                                                                            Find Unsteady aerodynamics at online marketplaces:


                                                                            46Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies

                                                                            By

                                                                            “Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies” Metadata:

                                                                            • Title: ➤  Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies
                                                                            • Author:
                                                                            • Language: English
                                                                            • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                                                            • Publish Date:
                                                                            • Publish Location: [Springfield, Va - Hampton, Va

                                                                            “Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies” Subjects and Themes:

                                                                            Edition Identifiers:

                                                                            Access and General Info:

                                                                            • First Year Published: 1997
                                                                            • Is Full Text Available: No
                                                                            • Is The Book Public: No
                                                                            • Access Status: No_ebook

                                                                            Online Access

                                                                            Downloads Are Not Available:

                                                                            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                            Online Borrowing:

                                                                              Online Marketplaces

                                                                              Find Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies at online marketplaces:


                                                                              47Application of the pressure sensitive paint technique to steady and unsteady flow

                                                                              By

                                                                              “Application of the pressure sensitive paint technique to steady and unsteady flow” Metadata:

                                                                              • Title: ➤  Application of the pressure sensitive paint technique to steady and unsteady flow
                                                                              • Author:
                                                                              • Language: English
                                                                              • Publisher: ➤  Joint Institute for Aeronautics and Acoustics - National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                              • Publish Date:
                                                                              • Publish Location: ➤  [Washington, DC - [Stanford, Calif.?] - Springfield, Va

                                                                              “Application of the pressure sensitive paint technique to steady and unsteady flow” Subjects and Themes:

                                                                              Edition Identifiers:

                                                                              Access and General Info:

                                                                              • First Year Published: 1996
                                                                              • Is Full Text Available: No
                                                                              • Is The Book Public: No
                                                                              • Access Status: No_ebook

                                                                              Online Access

                                                                              Downloads Are Not Available:

                                                                              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                              Online Borrowing:

                                                                                Online Marketplaces

                                                                                Find Application of the pressure sensitive paint technique to steady and unsteady flow at online marketplaces:


                                                                                48Spurious frequencies as a result of numerical boundary treatments

                                                                                By

                                                                                “Spurious frequencies as a result of numerical boundary treatments” Metadata:

                                                                                • Title: ➤  Spurious frequencies as a result of numerical boundary treatments
                                                                                • Author:
                                                                                • Language: English
                                                                                • Publisher: ➤  Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
                                                                                • Publish Date:
                                                                                • Publish Location: Hampton, Va - [Springfield, Va

                                                                                “Spurious frequencies as a result of numerical boundary treatments” Subjects and Themes:

                                                                                Edition Identifiers:

                                                                                Access and General Info:

                                                                                • First Year Published: 1990
                                                                                • Is Full Text Available: No
                                                                                • Is The Book Public: No
                                                                                • Access Status: No_ebook

                                                                                Online Access

                                                                                Downloads Are Not Available:

                                                                                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                Online Borrowing:

                                                                                  Online Marketplaces

                                                                                  Find Spurious frequencies as a result of numerical boundary treatments at online marketplaces:


                                                                                  49USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics

                                                                                  By

                                                                                  “USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics” Metadata:

                                                                                  • Title: ➤  USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics
                                                                                  • Author:
                                                                                  • Language: English
                                                                                  • Number of Pages: Median: 97
                                                                                  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
                                                                                  • Publish Date:
                                                                                  • Publish Location: [Washington, D.C.]

                                                                                  “USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics” Subjects and Themes:

                                                                                  Edition Identifiers:

                                                                                  Access and General Info:

                                                                                  • First Year Published: 1986
                                                                                  • Is Full Text Available: No
                                                                                  • Is The Book Public: No
                                                                                  • Access Status: No_ebook

                                                                                  Online Access

                                                                                  Downloads Are Not Available:

                                                                                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                  Online Borrowing:

                                                                                    Online Marketplaces

                                                                                    Find USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics at online marketplaces:


                                                                                    50Axis switching and spreading of an asymmetric jet

                                                                                    By

                                                                                    “Axis switching and spreading of an asymmetric jet” Metadata:

                                                                                    • Title: ➤  Axis switching and spreading of an asymmetric jet
                                                                                    • Author:
                                                                                    • Language: English
                                                                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                                                    • Publish Date:
                                                                                    • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                                                                    “Axis switching and spreading of an asymmetric jet” Subjects and Themes:

                                                                                    Edition Identifiers:

                                                                                    Access and General Info:

                                                                                    • First Year Published: 1994
                                                                                    • Is Full Text Available: No
                                                                                    • Is The Book Public: No
                                                                                    • Access Status: No_ebook

                                                                                    Online Access

                                                                                    Downloads Are Not Available:

                                                                                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                    Online Borrowing:

                                                                                      Online Marketplaces

                                                                                      Find Axis switching and spreading of an asymmetric jet at online marketplaces: