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1Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors

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“Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors” Metadata:

  • Title: ➤  Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

“Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors” 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

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    2Self-similar compressible free vortices

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    “Self-similar compressible free vortices” Metadata:

    • Title: ➤  Self-similar compressible free vortices
    • Author:
    • Language: English
    • Publisher: ➤  Joint Institute for Aeronautics and Acoustics, Stanford University - National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - [Stanford, Calif.]

    “Self-similar compressible free vortices” 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

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      3Axisymmetric free shear flows with and without swirl

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      “Axisymmetric free shear flows with and without swirl” Metadata:

      • Title: ➤  Axisymmetric free shear flows with and without swirl
      • Author:
      • Language: English
      • Number of Pages: Median: 533
      • Publisher: ➤  Mechanical Engineering Dept., Imperial College of Science and Technology - University of London, Faculty of Engineering
      • Publish Date:
      • Publish Location: London

      “Axisymmetric free shear flows with and without swirl” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1980
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

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        4Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique

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        “Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique” Metadata:

        • Title: ➤  Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique
        • Author:
        • Language: English
        • Number of Pages: Median: 18
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautiacs - Old Dominion University Research Foundation
        • Publish Date:
        • Publish Location: ➤  Washington, D. C - Springfield, Va - Norfolk, Va - [Washington, DC

        “Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique” 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

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          5Numerical investigations in the backflow region of a vacuum plume

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          “Numerical investigations in the backflow region of a vacuum plume” Metadata:

          • Title: ➤  Numerical investigations in the backflow region of a vacuum plume
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - Alabama A&M University - National Aeronautics and Space Administration
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Washington, DC - Normal, Ala

          “Numerical investigations in the backflow region of a vacuum plume” 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

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            6Enhanced mixing of an axisymmetric jet by aerodynamic excitation

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            “Enhanced mixing of an axisymmetric jet by aerodynamic excitation” Metadata:

            • Title: ➤  Enhanced mixing of an axisymmetric jet by aerodynamic excitation
            • Author:
            • Language: English
            • Number of Pages: Median: 170
            • Publisher: ➤  Lewis Research Center - For sale by the National Technical Information Service
            • Publish Date:
            • Publish Location: ➤  Cleveland, Ohio - [Springfield, Va

            “Enhanced mixing of an axisymmetric jet by aerodynamic excitation” 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

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              7Computing axisymmetric jet screech tones using unstructured grids

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              “Computing axisymmetric jet screech tones using unstructured grids” Metadata:

              • Title: ➤  Computing axisymmetric jet screech tones using unstructured grids
              • Author:
              • Language: English
              • Publisher: ➤  National Technical Information Service [distributor - National Aeronautics and Space Administration, Glenn Research Center - Available from the NASA Center for Aerospace Information
              • Publish Date:
              • Publish Location: ➤  Hanover, MD - [Cleveland, Ohio] - Springfield, VA

              “Computing axisymmetric jet screech tones using unstructured grids” 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

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                8Computer program BL2D for solving two-dimensional and axisymmetric boundary layers

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                “Computer program BL2D for solving two-dimensional and axisymmetric boundary layers” Metadata:

                • Title: ➤  Computer program BL2D for solving two-dimensional and axisymmetric boundary layers
                • 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

                “Computer program BL2D for solving two-dimensional and axisymmetric boundary layers” 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

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                9Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions

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                “Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions” Metadata:

                • Title: ➤  Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions
                • Author:
                • Number of Pages: Median: 49
                • Publisher: ➤  Institute for Aerospace Studies - [Institute for Aerospace Studies]
                • Publish Date:
                • Publish Location: [Downsview, Ont.]

                “Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1965
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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                10Calculations of diffuser flows with an anisotropic K-[epsilon] model

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                “Calculations of diffuser flows with an anisotropic K-[epsilon] model” Metadata:

                • Title: ➤  Calculations of diffuser flows with an anisotropic K-[epsilon] model
                • Author:
                • Language: English
                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                • Publish Date:
                • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                “Calculations of diffuser flows with an anisotropic K-[epsilon] 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.

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                  11Three component laser Doppler measurements in an axisymmetric jet

                  By

                  “Three component laser Doppler measurements in an axisymmetric jet” Metadata:

                  • Title: ➤  Three component laser Doppler measurements in an axisymmetric jet
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                  • Publish Date:
                  • Publish Location: Hampton, Va

                  “Three component laser Doppler measurements in an axisymmetric jet” 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

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                  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.

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                    12Experimental study of vortex breakdown in a cylindrical, swirling flow

                    “Experimental study of vortex breakdown in a cylindrical, swirling flow” Metadata:

                    • Title: ➤  Experimental study of vortex breakdown in a cylindrical, swirling flow
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Joint Institute for Aeronautics and Acoustics, Stanford University - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
                    • Publish Date:
                    • Publish Location: ➤  Springfield, Va - [Stanford, Calif.] - [Washington, DC

                    “Experimental study of vortex breakdown in a cylindrical, swirling 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

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                      13On the conditions for resonance interactions of instability waves in the axisymmetric jet

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                      “On the conditions for resonance interactions of instability waves in the axisymmetric jet” Metadata:

                      • Title: ➤  On the conditions for resonance interactions of instability waves in the axisymmetric jet
                      • Author:
                      • Number of Pages: Median: 11
                      • Publisher: ICOMP
                      • Publish Date:
                      • Publish Location: Cleveland, Ohio

                      “On the conditions for resonance interactions of instability waves in the axisymmetric jet” 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

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                      14Comparison of 3D computation and experiment for non-axisymmetric nozzles

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                      “Comparison of 3D computation and experiment for non-axisymmetric nozzles” Metadata:

                      • Title: ➤  Comparison of 3D computation and experiment for non-axisymmetric nozzles
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                      • Publish Date:
                      • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                      “Comparison of 3D computation and experiment for non-axisymmetric nozzles” 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

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                        15The flow induced by the coalescence of two initially stationary drops

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                        “The flow induced by the coalescence of two initially stationary drops” Metadata:

                        • Title: ➤  The flow induced by the coalescence of two initially stationary drops
                        • 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

                        “The flow induced by the coalescence of two initially stationary drops” 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

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                          16Model of an aero-space plane based on an idealized cone-derived waverider forebody

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                          “Model of an aero-space plane based on an idealized cone-derived waverider forebody” Metadata:

                          • Title: ➤  Model of an aero-space plane based on an idealized cone-derived waverider forebody
                          • Author:
                          • Number of Pages: Median: 146
                          • Publisher: University of Oklahoma
                          • Publish Date:
                          • Publish Location: Norman, Okla

                          “Model of an aero-space plane based on an idealized cone-derived waverider forebody” 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

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                          17Rapid numerical simulation of viscous axisymmetric flow fields

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                          “Rapid numerical simulation of viscous axisymmetric flow fields” Metadata:

                          • Title: ➤  Rapid numerical simulation of viscous axisymmetric flow fields
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                          • Publish Date:
                          • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                          “Rapid numerical simulation of viscous axisymmetric flow fields” 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

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                            18Comparison of turbulence models for nozzle-afterbody flows with propulsive jets

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                            “Comparison of turbulence models for nozzle-afterbody flows with propulsive jets” Metadata:

                            • Title: ➤  Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
                            • 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

                            “Comparison of turbulence models for nozzle-afterbody flows with propulsive jets” 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

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                              19An outflow boundary condition for aeroacoustic computations

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                              “An outflow boundary condition for aeroacoustic computations” Metadata:

                              • Title: ➤  An outflow boundary condition for aeroacoustic computations
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion
                              • Publish Date:
                              • Publish Location: ➤  Cleveland, Ohio - [Springfield, Va

                              “An outflow boundary condition for aeroacoustic computations” 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

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                              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.

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                                20The inviscid axisymmetric stability of the supersonic flow along a circular cylinder

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                                “The inviscid axisymmetric stability of the supersonic flow along a circular cylinder” Metadata:

                                • Title: ➤  The inviscid axisymmetric stability of the supersonic flow along a circular cylinder
                                • 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: [Springfield, Va - Hampton, VA

                                “The inviscid axisymmetric stability of the supersonic flow along a circular cylinder” 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

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                                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.

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                                  21On the interaction of Tollmien-Schlichting waves in axisymmetric supersonic flows

                                  By

                                  “On the interaction of Tollmien-Schlichting waves in axisymmetric supersonic flows” Metadata:

                                  • Title: ➤  On the interaction of Tollmien-Schlichting waves in axisymmetric supersonic flows
                                  • Author:
                                  • Number of Pages: Median: 18
                                  • Publisher: ICASE
                                  • Publish Date:
                                  • Publish Location: Hampton, Va

                                  “On the interaction of Tollmien-Schlichting waves in axisymmetric supersonic flows” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 1988
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  22Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability

                                  By

                                  “Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability” Metadata:

                                  • Title: ➤  Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
                                  • Publish Date:
                                  • Publish Location: ➤  [Springfield, Va - Washington, D.C

                                  “Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability” 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

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                                    23Supersonic jet noise reductions predicted with increased jet spreading rate

                                    By

                                    “Supersonic jet noise reductions predicted with increased jet spreading rate” Metadata:

                                    • Title: ➤  Supersonic jet noise reductions predicted with increased jet spreading rate
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                    • Publish Date:
                                    • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                    “Supersonic jet noise reductions predicted with increased jet spreading rate” 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

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                                      24Calculations of diffuser flows with an anisotropic K-[epsilon] model

                                      By

                                      “Calculations of diffuser flows with an anisotropic K-[epsilon] model” Metadata:

                                      • Title: ➤  Calculations of diffuser flows with an anisotropic K-[epsilon] model
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                      • Publish Date:
                                      • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                      “Calculations of diffuser flows with an anisotropic K-[epsilon] 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.

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                                        25Hydrodynamic calculations of axisymmetric accretion flow

                                        By

                                        “Hydrodynamic calculations of axisymmetric accretion flow” Metadata:

                                        • Title: ➤  Hydrodynamic calculations of axisymmetric accretion flow
                                        • Author:
                                        • Number of Pages: Median: 20
                                        • Publisher: ➤  Gasdynamics Laboratory, Dept. of Aeronautical Engineering, Faculty of Engineering, Kyoto University
                                        • Publish Date:
                                        • Publish Location: Kyoto

                                        “Hydrodynamic calculations of axisymmetric accretion flow” 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

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                                        26Studies of ion drift in axisymmetric flow fields

                                        By

                                        “Studies of ion drift in axisymmetric flow fields” Metadata:

                                        • Title: ➤  Studies of ion drift in axisymmetric flow fields
                                        • Author:
                                        • Publisher: ➤  Dept. of Aerospace Science and Engineering
                                        • Publish Date:
                                        • Publish Location: [Downsview, Ont.]

                                        “Studies of ion drift in axisymmetric flow fields” Subjects and Themes:

                                        Edition Identifiers:

                                        Access and General Info:

                                        • First Year Published: 1976
                                        • Is Full Text Available: No
                                        • Is The Book Public: No
                                        • Access Status: No_ebook

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                                        27The design/analysis of flows through turbomachinery

                                        By

                                        “The design/analysis of flows through turbomachinery” Metadata:

                                        • Title: ➤  The design/analysis of flows through turbomachinery
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  For sale by the National Technical Information Service - NASA
                                        • Publish Date:
                                        • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                        “The design/analysis of flows through turbomachinery” 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

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                                          28Inlet flow test calibration for a small axial compressor rig

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                                          “Inlet flow test calibration for a small axial compressor rig” Metadata:

                                          • Title: ➤  Inlet flow test calibration for a small axial compressor rig
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                          • Publish Date:
                                          • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                          “Inlet flow test calibration for a small axial compressor rig” Subjects and Themes:

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                                          • First Year Published: 1995
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                                            29Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation

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                                            “Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation” Metadata:

                                            • Title: ➤  Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation
                                            • Author:
                                            • Number of Pages: Median: 311
                                            • Publisher: Pineridge
                                            • Publish Date:
                                            • Publish Location: Swansea, U. K

                                            “Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation” Subjects and Themes:

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                                            • First Year Published: 1991
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                                            30Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation

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                                            “Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation” Metadata:

                                            • Title: ➤  Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
                                            • Publish Date:
                                            • Publish Location: ➤  Cleveland, Ohio - [Springfield, Va

                                            “Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation” Subjects and Themes:

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                                            • First Year Published: 1989
                                            • Is Full Text Available: No
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                                              31Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability

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                                              “Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability” Metadata:

                                              • Title: ➤  Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
                                              • Publish Date:
                                              • Publish Location: ➤  Springfield, Va - [Washington, D.C.]

                                              “Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability” Subjects and Themes:

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                                              • First Year Published: 1986
                                              • Is Full Text Available: No
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                                                32Numerical simulations of the flow in the HYPULSE expansion tube

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                                                “Numerical simulations of the flow in the HYPULSE expansion tube” Metadata:

                                                • Title: ➤  Numerical simulations of the flow in the HYPULSE expansion tube
                                                • Author:
                                                • Language: English
                                                • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                                                • Publish Date:
                                                • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                                                “Numerical simulations of the flow in the HYPULSE expansion tube” Subjects and Themes:

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                                                • First Year Published: 1995
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                                                  33The filtered Abel transform and its application in combustion diagnostics

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                                                  “The filtered Abel transform and its application in combustion diagnostics” Metadata:

                                                  • Title: ➤  The filtered Abel transform and its application in combustion diagnostics
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  National Technical Information Service [distributor - Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
                                                  • Publish Date:
                                                  • Publish Location: ➤  [Cleveland, Ohio] - Springfield, VA - Hanover, MD

                                                  “The filtered Abel transform and its application in combustion diagnostics” Subjects and Themes:

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                                                  • First Year Published: 2003
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                                                    34Marangoni convection in a gravity-free silicon float zone

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                                                    “Marangoni convection in a gravity-free silicon float zone” Metadata:

                                                    • Title: ➤  Marangoni convection in a gravity-free silicon float zone
                                                    • Author:
                                                    • Language: English
                                                    • Publisher: ➤  National Aeronautics and Space Administration - Carderock Division, Naval Surface Warfare Center - National Technical Information Service, distributor
                                                    • Publish Date:
                                                    • Publish Location: ➤  Bethesda, Md - Springfield, Va - [Washington, DC

                                                    “Marangoni convection in a gravity-free silicon float zone” Subjects and Themes:

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                                                    • First Year Published: 1994
                                                    • Is Full Text Available: No
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                                                      35Spreading characteristics and thrust of jets from asymmetric nozzles

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                                                      “Spreading characteristics and thrust of jets from asymmetric nozzles” Metadata:

                                                      • Title: ➤  Spreading characteristics and thrust of jets from asymmetric nozzles
                                                      • Author:
                                                      • Language: English
                                                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                      • Publish Date:
                                                      • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                                      “Spreading characteristics and thrust of jets from asymmetric nozzles” Subjects and Themes:

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                                                      Access and General Info:

                                                      • First Year Published: 1995
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                                                        36Computations of axisymmetric flows in hypersonic shock tubes

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                                                        “Computations of axisymmetric flows in hypersonic shock tubes” Metadata:

                                                        • Title: ➤  Computations of axisymmetric flows in hypersonic shock tubes
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                                                        • 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 - Washington, DC

                                                        “Computations of axisymmetric flows in hypersonic shock tubes” Subjects and Themes:

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                                                        • First Year Published: 1995
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                                                          37Jets and flames in co-flowing streams

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                                                          “Jets and flames in co-flowing streams” Metadata:

                                                          • Title: ➤  Jets and flames in co-flowing streams
                                                          • Author:
                                                          • Publisher: AIAA
                                                          • Publish Date:
                                                          • Publish Location: New York

                                                          “Jets and flames in co-flowing streams” Subjects and Themes:

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                                                          Access and General Info:

                                                          • First Year Published: 1987
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                                                          38Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks

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                                                          “Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks” Metadata:

                                                          • Title: ➤  Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                          • Publish Date:
                                                          • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                                          “Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks” Subjects and Themes:

                                                          Edition Identifiers:

                                                          Access and General Info:

                                                          • First Year Published: 1995
                                                          • Is Full Text Available: No
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                                                            39An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies

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                                                            “An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies” Metadata:

                                                            • Title: ➤  An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies
                                                            • Author:
                                                            • Language: English
                                                            • Publisher: ➤  National Aeronautics and Space Administration, Lyndon B. Johnson Space Center - National Technical Information Service, distributor
                                                            • Publish Date:
                                                            • Publish Location: ➤  [Springfield, Va - Houston, Tex

                                                            “An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies” Subjects and Themes:

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                                                            • First Year Published: 1998
                                                            • Is Full Text Available: No
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                                                              Wiki

                                                              Source: Wikipedia

                                                              Wikipedia Results

                                                              Search Results from Wikipedia

                                                              Navier–Stokes equations

                                                              for creeping flow results when the left side is assumed zero. In axisymmetric flow another stream function formulation, called the Stokes stream function

                                                              Stokes' law

                                                              flow direction, while r is the radius as measured perpendicular to the z–axis. The origin is at the sphere centre. Because the flow is axisymmetric around

                                                              Beltrami flow

                                                              immediate consequence of Beltrami flow is that it can never be a planar or axisymmetric flow because in those flows, vorticity is always perpendicular

                                                              Taylor–Couette flow

                                                              and a secondary steady state characterized by axisymmetric toroidal vortices, known as Taylor vortex flow, emerges. Subsequently, upon increasing the angular

                                                              Fredholm integral equation

                                                              PMID 10060625. Daddi-Moussa-Ider, A.; Kaoui, B.; Löwen, H. (9 April 2019). "Axisymmetric flow due to a Stokeslet near a finite-sized elastic membrane". Journal

                                                              Taylor–Culick flow

                                                              In fluid dynamics, Taylor–Culick flow, a type of a stagnation point flow, describes the axisymmetric flow inside a long slender cylinder with one end closed

                                                              Hagen–Poiseuille equation

                                                              The flow is steady ( ⁠∂.../∂t⁠ = 0 ). The radial and azimuthal components of the fluid velocity are zero ( ur = uθ = 0 ). The flow is axisymmetric ( ⁠∂

                                                              Stagnation point flow

                                                              equipment. The axisymmetric stagnation point flow corresponds to α = β ( λ = 0 ) {\displaystyle \alpha =\beta \,(\lambda =0)} . The flow field can be simply

                                                              Waverider

                                                              Axisymmetric Flow Fields". Ingenieur-Archiv, 37, Band, 1, Heft, pp. 56-72, 1968. Pike, J. (1–3 May 1968). Experimental Results from Three Cone-Flow Waveriders

                                                              Centrifugal compressor

                                                              sub-class of dynamic, axisymmetric, work-absorbing turbomachinery. They achieve pressure rise by adding energy to the continuous flow of fluid through the