Explore: Engine Inlets

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1Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems

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“Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems” Metadata:

  • Title: ➤  Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Technical Information Service [distributor - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  [Washington, DC - Springfield, Va

“Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems” 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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    2Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip

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    “Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip” Metadata:

    • Title: ➤  Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: [Washington, D.C.]

    “Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip” 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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      3Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations

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      “Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations” Metadata:

      • Title: ➤  Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  [Washington, DC - Springfield, Va

      “Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations” 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

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        4IPAC--Inlet Performance Analysis Code

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        “IPAC--Inlet Performance Analysis Code” Metadata:

        • Title: ➤  IPAC--Inlet Performance Analysis Code
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - [Washington, DC

        “IPAC--Inlet Performance Analysis Code” 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

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          5Performance study for inlet installations

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          “Performance study for inlet installations” Metadata:

          • Title: ➤  Performance study for inlet installations
          • 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

          “Performance study for inlet installations” 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:

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            6Rocket-based combined cycle engine technology development

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            “Rocket-based combined cycle engine technology development” Metadata:

            • Title: ➤  Rocket-based combined cycle engine technology development
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion - National Aeronautics and Space Administration, distributor]
            • Publish Date:
            • Publish Location: ➤  [Cleveland, Ohio] - [Springfield, Va

            “Rocket-based combined cycle engine technology development” 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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              7NASA Lewis Propulsion Systems Laboratory customer guide manual

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              “NASA Lewis Propulsion Systems Laboratory customer guide manual” Metadata:

              • Title: ➤  NASA Lewis Propulsion Systems Laboratory customer guide manual
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: ➤  [Springfield, Va - [Washington, DC]

              “NASA Lewis Propulsion Systems Laboratory customer guide manual” 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:

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                8Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow

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                “Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow” Metadata:

                • Title: ➤  Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                • Publish Date:
                • Publish Location: ➤  [Washington, D.C - Springfield, Va

                “Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with 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

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                  9An investigation of bleed configurations and their effect on shock wave/boundary layer interactions

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                  “An investigation of bleed configurations and their effect on shock wave/boundary layer interactions” Metadata:

                  • Title: ➤  An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - University of Cincinnati - National Aeronautics and Space Administration
                  • Publish Date:
                  • Publish Location: ➤  Springfield, Va - [Cincinnati, Ohio?] - [Washington, DC

                  “An investigation of bleed configurations and their effect on shock wave/boundary layer interactions” 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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                    10Comparison of the aeroacoustics of two small-scale supersonic inlets

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                    “Comparison of the aeroacoustics of two small-scale supersonic inlets” Metadata:

                    • Title: ➤  Comparison of the aeroacoustics of two small-scale supersonic inlets
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                    • Publish Date:
                    • Publish Location: ➤  Springfield, Va - [Washington, DC

                    “Comparison of the aeroacoustics of two small-scale supersonic inlets” 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:

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                      11Control of flow separation and mixing by aerodynamic excitation

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                      “Control of flow separation and mixing by aerodynamic excitation” Metadata:

                      • Title: ➤  Control of flow separation and mixing by aerodynamic excitation
                      • Author:
                      • Language: English
                      • Number of Pages: Median: 11
                      • Publisher: ➤  NASA - For sale by the National Technical Information Service
                      • Publish Date:
                      • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                      “Control of flow separation and mixing by aerodynamic excitation” 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

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                        12Mach 10 experimental database of a three-dimensional scramjet inlet flow field

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                        “Mach 10 experimental database of a three-dimensional scramjet inlet flow field” Metadata:

                        • Title: ➤  Mach 10 experimental database of a three-dimensional scramjet inlet flow field
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 214
                        • Publisher: ➤  Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
                        • Publish Date:
                        • Publish Location: ➤  Hampton, Va - [Springfield, VA - Springfield, VA

                        “Mach 10 experimental database of a three-dimensional scramjet inlet flow field” 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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                          133D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

                          By

                          “3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:

                          • Title: ➤  3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                          • Publish Date:
                          • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                          “3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” 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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                            14Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet

                            By

                            “Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet” Metadata:

                            • Title: ➤  Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                            • Publish Date:
                            • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                            “Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet” 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.

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                              15Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet

                              By

                              “Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet” Metadata:

                              • Title: ➤  Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                              • Publish Date:
                              • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                              “Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet” 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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                                Find Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet at online marketplaces:


                                16Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

                                By

                                “Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Metadata:

                                • Title: ➤  Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
                                • 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

                                “Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” 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.

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                                  173D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

                                  By

                                  “3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:

                                  • Title: ➤  3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                  • Publish Date:
                                  • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                  “3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” 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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                                    18Finite difference time marching in the frequency domain

                                    By

                                    “Finite difference time marching in the frequency domain” Metadata:

                                    • Title: ➤  Finite difference time marching in the frequency domain
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                    • Publish Date:
                                    • Publish Location: ➤  [Washington, D.C - Springfield, Va - [Washington, DC

                                    “Finite difference time marching in the frequency domain” 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.

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                                      19Multigrid methods for aerodynamic problems in complex geometries

                                      By

                                      “Multigrid methods for aerodynamic problems in complex geometries” Metadata:

                                      • Title: ➤  Multigrid methods for aerodynamic problems in complex geometries
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                      • Publish Date:
                                      • Publish Location: ➤  Springfield, Va - [Washington, D.C

                                      “Multigrid methods for aerodynamic problems in complex geometries” 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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                                        20High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion

                                        By

                                        “High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion” Metadata:

                                        • Title: ➤  High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion
                                        • Author:
                                        • Language: English
                                        • Number of Pages: Median: 165
                                        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                                        • Publish Date:
                                        • Publish Location: Hampton, Va

                                        “High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion” Subjects and Themes:

                                        Edition Identifiers:

                                        Access and General Info:

                                        • First Year Published: 2005
                                        • 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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                                          21Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach

                                          By

                                          “Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach” Metadata:

                                          • Title: ➤  Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                          • Publish Date:
                                          • Publish Location: ➤  Springfield, Va - [Washington, DC

                                          “Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach” 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:

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                                            22Application of CFD to the analysis and design of high-speed inlets

                                            By

                                            “Application of CFD to the analysis and design of high-speed inlets” Metadata:

                                            • Title: ➤  Application of CFD to the analysis and design of high-speed inlets
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                            • Publish Date:
                                            • Publish Location: ➤  Springfield, Va - [Washington, DC

                                            “Application of CFD to the analysis and design of high-speed inlets” 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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                                              23SSME fuelside preburner two-dimensional analysis

                                              By

                                              “SSME fuelside preburner two-dimensional analysis” Metadata:

                                              • Title: ➤  SSME fuelside preburner two-dimensional analysis
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
                                              • Publish Date:
                                              • Publish Location: [Cleveland, Ohio

                                              “SSME fuelside preburner two-dimensional 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.

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                                                24Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

                                                By

                                                “Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Metadata:

                                                • Title: ➤  Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
                                                • 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

                                                “Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” 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.

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                                                  25Three 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:

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                                                  • First Year Published: 1994
                                                  • Is Full Text Available: No
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                                                    26Fan noise prediction assessment

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                                                    “Fan noise prediction assessment” Metadata:

                                                    • Title: ➤  Fan noise prediction assessment
                                                    • 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

                                                    “Fan noise prediction assessment” Subjects and Themes:

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                                                    Access and General Info:

                                                    • First Year Published: 1995
                                                    • Is Full Text Available: No
                                                    • Is The Book Public: No
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                                                      27Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft

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                                                      “Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft” Metadata:

                                                      • Title: ➤  Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft
                                                      • Author:
                                                      • Language: English
                                                      • Publisher: ➤  The Center - National Technical Information Service, distributor
                                                      • Publish Date:
                                                      • Publish Location: ➤  Cleveland, OH - [Springfield, Va

                                                      “Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft” Subjects and Themes:

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                                                      • First Year Published: 1994
                                                      • Is Full Text Available: No
                                                      • Is The Book Public: No
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                                                        28Fan noise prediction system development

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                                                        “Fan noise prediction system development” Metadata:

                                                        • Title: ➤  Fan noise prediction system development
                                                        • Author:
                                                        • Language: English
                                                        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                        • Publish Date:
                                                        • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                        “Fan noise prediction system development” Subjects and Themes:

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                                                        • First Year Published: 1993
                                                        • Is Full Text Available: No
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                                                          29Improved finite element modeling of the turbofan engine inlet radiation problem

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                                                          “Improved finite element modeling of the turbofan engine inlet radiation problem” Metadata:

                                                          • Title: ➤  Improved finite element modeling of the turbofan engine inlet radiation problem
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                          • Publish Date:
                                                          • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                          “Improved finite element modeling of the turbofan engine inlet radiation problem” Subjects and Themes:

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                                                          • First Year Published: 1993
                                                          • Is Full Text Available: No
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                                                            30Effects of initial conditions on a single jet in crossflow

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                                                            • Title: ➤  Effects of initial conditions on a single jet in crossflow
                                                            • Author:
                                                            • Language: English
                                                            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                            • Publish Date:
                                                            • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                                            “Effects of initial conditions on a single jet in crossflow” Subjects and Themes:

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                                                            • First Year Published: 1995
                                                            • Is Full Text Available: No
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                                                              31Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers

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                                                              “Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers” Metadata:

                                                              • Title: ➤  Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
                                                              • Author:
                                                              • Language: English
                                                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
                                                              • Publish Date:
                                                              • Publish Location: ➤  [Cleveland, Ohio] - [Springfield, Va

                                                              “Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers” Subjects and Themes:

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                                                              • First Year Published: 1999
                                                              • Is Full Text Available: No
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                                                                32Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack

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                                                                “Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack” Metadata:

                                                                • Title: ➤  Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
                                                                • Author:
                                                                • Language: English
                                                                • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                • Publish Date:
                                                                • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                                                “Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack” Subjects and Themes:

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                                                                • First Year Published: 1995
                                                                • Is Full Text Available: No
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                                                                  33PARC3D calculations of the F/A-18A HARV inlet vortex generators

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                                                                  “PARC3D calculations of the F/A-18A HARV inlet vortex generators” Metadata:

                                                                  • Title: ➤  PARC3D calculations of the F/A-18A HARV inlet vortex generators
                                                                  • Author:
                                                                  • Language: English
                                                                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                  • Publish Date:
                                                                  • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                                                  “PARC3D calculations of the F/A-18A HARV inlet vortex generators” Subjects and Themes:

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                                                                  • First Year Published: 1995
                                                                  • Is Full Text Available: No
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                                                                    34Computational analysis in support of the SSTO flowpath test

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                                                                    “Computational analysis in support of the SSTO flowpath test” Metadata:

                                                                    • Title: ➤  Computational analysis in support of the SSTO flowpath test
                                                                    • Author:
                                                                    • Language: English
                                                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                                    • Publish Date:
                                                                    • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                                                    “Computational analysis in support of the SSTO flowpath test” Subjects and Themes:

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                                                                    • First Year Published: 1994
                                                                    • Is Full Text Available: No
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                                                                      35A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics

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                                                                      “A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics” Metadata:

                                                                      • Title: ➤  A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics
                                                                      • Author:
                                                                      • Language: English
                                                                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                      • Publish Date:
                                                                      • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                                                      “A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics” Subjects and Themes:

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                                                                      • First Year Published: 1991
                                                                      • Is Full Text Available: No
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                                                                        36A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

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                                                                        “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:

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                                                                        • First Year Published: 1996
                                                                        • Is Full Text Available: No
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                                                                          37Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines

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                                                                          “Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines” Metadata:

                                                                          • Title: ➤  Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines
                                                                          • Author:
                                                                          • Language: English
                                                                          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                          • Publish Date:
                                                                          • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                                                          “Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines” Subjects and Themes:

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                                                                          • First Year Published: 1995
                                                                          • Is Full Text Available: No
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                                                                            38A numerical analysis applied to high angle of attack three-dimensional inlets

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                                                                            “A numerical analysis applied to high angle of attack three-dimensional inlets” Metadata:

                                                                            • Title: ➤  A numerical analysis applied to high angle of attack three-dimensional inlets
                                                                            • Author:
                                                                            • Language: English
                                                                            • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
                                                                            • Publish Date:
                                                                            • Publish Location: [Cleveland, Ohio

                                                                            “A numerical analysis applied to high angle of attack three-dimensional inlets” Subjects and Themes:

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                                                                            • First Year Published: 1986
                                                                            • Is Full Text Available: No
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