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1Numerical simulation of shock/turbulent boundary layer interaction

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“Numerical simulation of shock/turbulent boundary layer interaction” Metadata:

  • Title: ➤  Numerical simulation of shock/turbulent boundary layer interaction
  • Author:
  • Language: English
  • Publisher: ➤  Dept. of Aerospace Engineering Sciences, University of Colorado - National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C - Boulder, Colo - Springfield, Va

“Numerical simulation of shock/turbulent boundary layer interaction” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1993
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    23-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions

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    “3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions” Metadata:

    • Title: ➤  3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: ➤  [Washington, DC] - [Springfield, Va

    “3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions” 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

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      3Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction

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      “Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” Metadata:

      • Title: ➤  Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - Austin, Tex - [Washington, DC

      “Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” 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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        4An 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

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          5Flow characteristics in boundary layer bleed slots with plenum

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          “Flow characteristics in boundary layer bleed slots with plenum” Metadata:

          • Title: ➤  Flow characteristics in boundary layer bleed slots with plenum
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Washington, D.C

          “Flow characteristics in boundary layer bleed slots with plenum” 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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            6A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction

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            “A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction” Metadata:

            • Title: ➤  A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction
            • Author:
            • Language: English
            • Number of Pages: Median: 17
            • 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: ➤  [Washington, D.C.] - Springfield, Va

            “A time-accurate adaptive grid method and the numerical simulation of shock-vortex interaction” 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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              7Simulation of January 1-7, 1978 events

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              “Simulation of January 1-7, 1978 events” Metadata:

              • Title: ➤  Simulation of January 1-7, 1978 events
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: ➤  [Washington, DC - Springfield, Va

              “Simulation of January 1-7, 1978 events” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

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

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                8Mach 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

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                  9Blockage development in a transonic, axial compressor rotor

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                  “Blockage development in a transonic, axial compressor rotor” Metadata:

                  • Title: ➤  Blockage development in a transonic, axial compressor rotor
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                  • Publish Date:
                  • Publish Location: ➤  [Washington, D.C - Springfield, Va

                  “Blockage development in a transonic, axial compressor rotor” 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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                    10Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor

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                    “Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor” Metadata:

                    • Title: ➤  Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                    • Publish Date:
                    • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                    “Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor” 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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                      113D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

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                      “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

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                        12Hypersonic flows as related to the national aerospace plane

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                        “Hypersonic flows as related to the national aerospace plane” Metadata:

                        • Title: ➤  Hypersonic flows as related to the national aerospace plane
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 57
                        • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - Eloret Institute - For sale by the National Technical Information Service
                        • Publish Date:
                        • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif - Sunnyvale, Calif

                        “Hypersonic flows as related to the national aerospace plane” 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

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                          13Motion of the heliospheric termination shock

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                          “Motion of the heliospheric termination shock” Metadata:

                          • Title: ➤  Motion of the heliospheric termination shock
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                          • Publish Date:
                          • Publish Location: ➤  [Washington, DC - Springfield, Va

                          “Motion of the heliospheric termination shock” 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

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                            14Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

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                            “Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code” Metadata:

                            • Title: ➤  Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                            • Publish Date:
                            • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                            “Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code” 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

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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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                              15Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions

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                              “Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions” Metadata:

                              • Title: ➤  Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                              • Publish Date:
                              • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                              “Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions” 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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                                16Numerical simulation of low-density shock-wave interactions

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                                “Numerical simulation of low-density shock-wave interactions” Metadata:

                                • Title: ➤  Numerical simulation of low-density shock-wave interactions
                                • 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

                                “Numerical simulation of low-density shock-wave interactions” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

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

                                Online Access

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                                  17Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

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                                  “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

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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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                                    18Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction

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                                    “Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction” Metadata:

                                    • Title: ➤  Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
                                    • Publish Date:
                                    • Publish Location: ➤  [Cleveland, Ohio] - Springfield, VA

                                    “Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

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

                                    Online Access

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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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                                      19Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction

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                                      “Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction” Metadata:

                                      • Title: ➤  Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction
                                      • Author:
                                      • Language: English
                                      • Number of Pages: Median: 18
                                      • Publisher: ➤  Lewis Research Center - National Aeronautics and Space Administration - National Technical Information Service, distributor
                                      • Publish Date:
                                      • Publish Location: ➤  Cleveland, Ohio - [Springfield, Va - [Washington, DC]

                                      “Surface and flow field measurements in a symmetric crossing shock wave/turbulent boundary-layer interaction” 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

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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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                                        203D 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

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                                          21Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids

                                          By

                                          “Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids” Metadata:

                                          • Title: ➤  Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids
                                          • 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

                                          “Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids” 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

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                                            22Laser light scattering by shock waves

                                            By

                                            “Laser light scattering by shock waves” Metadata:

                                            • Title: ➤  Laser light scattering by shock waves
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                            • Publish Date:
                                            • Publish Location: ➤  [Washington, D.C - Springfield, Va

                                            “Laser light scattering by shock waves” 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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                                              23An analytical and numerical study of a shock wave interaction with an area change

                                              By

                                              “An analytical and numerical study of a shock wave interaction with an area change” Metadata:

                                              • Title: ➤  An analytical and numerical study of a shock wave interaction with an area change
                                              • Author:
                                              • Publisher: ➤  Dept. of Aerospace Science and Engineering - Institute for Aerospace Studies
                                              • Publish Date:
                                              • Publish Location: [Downsview, Ont.]

                                              “An analytical and numerical study of a shock wave interaction with an area change” Subjects and Themes:

                                              Edition Identifiers:

                                              Access and General Info:

                                              • First Year Published: 1982
                                              • Is Full Text Available: No
                                              • Is The Book Public: No
                                              • Access Status: No_ebook

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                                              24Flow separation in shock wave boundary layer interactions at hypersonic speeds

                                              By

                                              “Flow separation in shock wave boundary layer interactions at hypersonic speeds” Metadata:

                                              • Title: ➤  Flow separation in shock wave boundary layer interactions at hypersonic speeds
                                              • 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

                                              “Flow separation in shock wave boundary layer interactions at hypersonic speeds” 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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                                                25Studies of shock wave interactions with homogeneous and isotropic turbulence

                                                “Studies of shock wave interactions with homogeneous and isotropic turbulence” Metadata:

                                                • Title: ➤  Studies of shock wave interactions with homogeneous and isotropic turbulence
                                                • Language: English
                                                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                                • Publish Date:
                                                • Publish Location: Hampton, Va - Springfield, VA

                                                “Studies of shock wave interactions with homogeneous and isotropic turbulence” Subjects and Themes:

                                                Edition Identifiers:

                                                Access and General Info:

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

                                                Online Access

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                                                  26The design and development of a wave interaction tube for the study of non-linear waves

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                                                  “The design and development of a wave interaction tube for the study of non-linear waves” Metadata:

                                                  • Title: ➤  The design and development of a wave interaction tube for the study of non-linear waves
                                                  • Author:
                                                  • Number of Pages: Median: 184
                                                  • Publisher: [Institute of Aerophysics]
                                                  • Publish Date:
                                                  • Publish Location: [Downsview, Ont.]

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                                                  27A time-accurate adaptive grid method and the numerical simulation of a shock-vortex interaction

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                                                  “A time-accurate adaptive grid method and the numerical simulation of a shock-vortex interaction” Metadata:

                                                  • Title: ➤  A time-accurate adaptive grid method and the numerical simulation of a shock-vortex interaction
                                                  • Author:
                                                  • Number of Pages: Median: 17
                                                  • Publisher: Langley Research Center
                                                  • Publish Date:
                                                  • Publish Location: Hampton, Va

                                                  “A time-accurate adaptive grid method and the numerical simulation of a shock-vortex interaction” Subjects and Themes:

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                                                  28Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream

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                                                  “Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Metadata:

                                                  • Title: ➤  Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                  • Publish Date:
                                                  • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                                  “Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Subjects and Themes:

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                                                    29A numerical study of fundamental shock noise mechanisms

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                                                    • Title: ➤  A numerical study of fundamental shock noise mechanisms
                                                    • Author:
                                                    • Language: English
                                                    • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration
                                                    • Publish Date:
                                                    • Publish Location: ➤  [Washington, D.C - Springfield, Va

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                                                      30Numerical calculations of shock-wave/boundary-layer flow interactions

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                                                      • Title: ➤  Numerical calculations of shock-wave/boundary-layer flow interactions
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                                                      • Language: English
                                                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                      • Publish Date:
                                                      • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                                      “Numerical calculations of shock-wave/boundary-layer flow interactions” Subjects and Themes:

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                                                        31Interaction of a shock with a longitudinal vortex

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                                                        • Title: ➤  Interaction of a shock with a longitudinal vortex
                                                        • Author:
                                                        • Language: English
                                                        • Publisher: ➤  National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
                                                        • Publish Date:
                                                        • Publish Location: [Springfield, Va - Hampton, VA

                                                        “Interaction of a shock with a longitudinal vortex” Subjects and Themes:

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                                                          32A Cartesian grid approach with hierarchical refinement for compressible flows

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                                                          • Title: ➤  A Cartesian grid approach with hierarchical refinement for compressible flows
                                                          • 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

                                                          “A Cartesian grid approach with hierarchical refinement for compressible flows” Subjects and Themes:

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                                                            33On the dynamics of a shock-bubble interaction

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                                                            • Title: ➤  On the dynamics of a shock-bubble interaction
                                                            • 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

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                                                              34The design of a wave interaction tube

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                                                              • Title: ➤  The design of a wave interaction tube
                                                              • Author:
                                                              • Number of Pages: Median: 136
                                                              • Publisher: Institute for Aerophysics
                                                              • Publish Date:
                                                              • Publish Location: [Downsview, Ont.]

                                                              “The design of a wave interaction tube” Subjects and Themes:

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                                                              • First Year Published: 1950
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                                                              35Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

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                                                              • 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:

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                                                                36Low dissipative high order shock-capturing methods using characteristic-based filters

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                                                                • Title: ➤  Low dissipative high order shock-capturing methods using characteristic-based filters
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                                                                • Language: English
                                                                • Publisher: ➤  National Technical Information Service, distributor - Research Institute for Advanced Computer Science, NASA Ames Research Center
                                                                • Publish Date:
                                                                • Publish Location: ➤  [Moffett Field, Calif.] - [Springfield, Va

                                                                “Low dissipative high order shock-capturing methods using characteristic-based filters” Subjects and Themes:

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                                                                • First Year Published: 1998
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                                                                  37Effect of fin leading edge sweep on shock-shock interaction at Mach 6

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                                                                  “Effect of fin leading edge sweep on shock-shock interaction at Mach 6” Metadata:

                                                                  • Title: ➤  Effect of fin leading edge sweep on shock-shock interaction at Mach 6
                                                                  • Author:
                                                                  • Language: English
                                                                  • Publisher: ➤  American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                  • Publish Date:
                                                                  • Publish Location: ➤  Springfield, Va - Washington, DC

                                                                  “Effect of fin leading edge sweep on shock-shock interaction at Mach 6” Subjects and Themes:

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                                                                    38Cylindrical sound wave generated by shock-vortex interaction

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                                                                    “Cylindrical sound wave generated by shock-vortex interaction” Metadata:

                                                                    • Title: ➤  Cylindrical sound wave generated by shock-vortex interaction
                                                                    • Author:
                                                                    • Number of Pages: Median: 1715
                                                                    • Publisher: Sine nomine
                                                                    • Publish Date:
                                                                    • Publish Location: [S.l.]

                                                                    “Cylindrical sound wave generated by shock-vortex interaction” Subjects and Themes:

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                                                                    • First Year Published: 1985
                                                                    • Is Full Text Available: No
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                                                                    39Spectrum of noise from shock-turbulence interaction

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                                                                    • Title: ➤  Spectrum of noise from shock-turbulence interaction
                                                                    • Author:
                                                                    • Publisher: Sine nomine
                                                                    • Publish Date:
                                                                    • Publish Location: [S.l.]

                                                                    “Spectrum of noise from shock-turbulence interaction” Subjects and Themes:

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                                                                    • First Year Published: 1986
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                                                                    40Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model

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                                                                    “Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model” Metadata:

                                                                    • Title: ➤  Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model
                                                                    • Author:
                                                                    • Language: English
                                                                    • Number of Pages: Median: 38
                                                                    • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration
                                                                    • Publish Date:
                                                                    • Publish Location: ➤  [Washington, D.C - Springfield, Va

                                                                    “Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model” Subjects and Themes:

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                                                                    • First Year Published: 1990
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                                                                      41Computational modeling and validation for hypersonic inlets

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                                                                      “Computational modeling and validation for hypersonic inlets” Metadata:

                                                                      • Title: ➤  Computational modeling and validation for hypersonic inlets
                                                                      • Author:
                                                                      • Language: English
                                                                      • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration
                                                                      • Publish Date:
                                                                      • Publish Location: ➤  [Washington, D.C - Springfield, Va

                                                                      “Computational modeling and validation for hypersonic inlets” Subjects and Themes:

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                                                                      • First Year Published: 1990
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                                                                        42Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10

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                                                                        “Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10” Metadata:

                                                                        • Title: ➤  Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
                                                                        • Author:
                                                                        • Language: English
                                                                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - NASA Center for AeroSpace Information, distributor
                                                                        • Publish Date:
                                                                        • Publish Location: ➤  Springfield, Va - Hampton, Va - Linthicum Heights, MD

                                                                        “Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10” Subjects and Themes:

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                                                                        • First Year Published: 1995
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                                                                          43Mach 10 computational study of a three-dimensional scramjet inlet flow field

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                                                                          “Mach 10 computational study of a three-dimensional scramjet inlet flow field” Metadata:

                                                                          • Title: ➤  Mach 10 computational study of a three-dimensional scramjet inlet flow field
                                                                          • 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

                                                                          “Mach 10 computational study of a three-dimensional scramjet inlet flow field” Subjects and Themes:

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                                                                          • First Year Published: 1995
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                                                                            44Weak-wave analysis of shock interaction with a slipstream

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                                                                            • Title: ➤  Weak-wave analysis of shock interaction with a slipstream
                                                                            • Author:
                                                                            • Number of Pages: Median: 17
                                                                            • Publisher: Langley Research Center
                                                                            • Publish Date:
                                                                            • Publish Location: Hampton, Va

                                                                            “Weak-wave analysis of shock interaction with a slipstream” Subjects and Themes:

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                                                                            • First Year Published: 1988
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                                                                            45Experimental studies of shock-wave/wall-jet interaction in hypersonic flow

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                                                                            “Experimental studies of shock-wave/wall-jet interaction in hypersonic flow” Metadata:

                                                                            • Title: ➤  Experimental studies of shock-wave/wall-jet interaction in hypersonic flow
                                                                            • 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

                                                                            “Experimental studies of shock-wave/wall-jet interaction in hypersonic flow” Subjects and Themes:

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                                                                            • First Year Published: 1994
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                                                                              46Shock wave interaction with an abrupt area change

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                                                                              • Title: ➤  Shock wave interaction with an abrupt area change
                                                                              • Author:
                                                                              • Language: English
                                                                              • Number of Pages: Median: 13
                                                                              • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                                                                              • Publish Date:
                                                                              • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                                                              “Shock wave interaction with an abrupt area change” Subjects and Themes:

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                                                                              • First Year Published: 1991
                                                                              • Is Full Text Available: No
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                                                                                47Numerical simulation of supersonic flow using a new analytical bleed boundary condition

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                                                                                • Title: ➤  Numerical simulation of supersonic flow using a new analytical bleed boundary condition
                                                                                • Author:
                                                                                • Language: English
                                                                                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                                                • Publish Date:
                                                                                • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                                                                “Numerical simulation of supersonic flow using a new analytical bleed boundary condition” Subjects and Themes:

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                                                                                • First Year Published: 1995
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                                                                                  48Interactive calculation procedures for mixed compression inlets

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                                                                                  “Interactive calculation procedures for mixed compression inlets” Metadata:

                                                                                  • Title: ➤  Interactive calculation procedures for mixed compression inlets
                                                                                  • Author:
                                                                                  • Language: English
                                                                                  • Publisher: ➤  Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University
                                                                                  • Publish Date:
                                                                                  • Publish Location: Cleveland, Ohio

                                                                                  “Interactive calculation procedures for mixed compression inlets” Subjects and Themes:

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                                                                                  • First Year Published: 1983
                                                                                  • Is Full Text Available: No
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                                                                                    49Interaction of oblique shock and detonation waves

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                                                                                    “Interaction of oblique shock and detonation waves” Metadata:

                                                                                    • Title: ➤  Interaction of oblique shock and detonation waves
                                                                                    • Author:
                                                                                    • Publisher: ➤  Institute for Aerospace Studies
                                                                                    • Publish Date:
                                                                                    • Publish Location: [Downsview, Ont.]

                                                                                    “Interaction of oblique shock and detonation waves” Subjects and Themes:

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                                                                                    • First Year Published: 1982
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                                                                                    50Numerical analysis of peak heat transfer rates for hypersonic flow over a cowl leading edge

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                                                                                    “Numerical analysis of peak heat transfer rates for hypersonic flow over a cowl leading edge” Metadata:

                                                                                    • Title: ➤  Numerical analysis of peak heat transfer rates for hypersonic flow over a cowl leading edge
                                                                                    • Author:
                                                                                    • Publisher: AIAA
                                                                                    • Publish Date:
                                                                                    • Publish Location: New York

                                                                                    “Numerical analysis of peak heat transfer rates for hypersonic flow over a cowl leading edge” Subjects and Themes:

                                                                                    Edition Identifiers:

                                                                                    Access and General Info:

                                                                                    • First Year Published: 1987
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                                                                                    Shock wave

                                                                                    In physics, a shock wave (also spelled shockwave), or shock, is a type of propagating disturbance that moves faster than the local speed of sound in the

                                                                                    Shock tube

                                                                                    the pyrotechnic initiator, see Shock tube detonator A shock tube is an instrument used to create and direct shock waves at a sensor or model in order to

                                                                                    Shock waves in astrophysics

                                                                                    shocks is still under investigation, but it is widely accepted that the general mechanism driving these shocks consists of wave particle interaction and

                                                                                    Bow shock

                                                                                    bow shocks are shock waves in regions where the conditions of density and pressure change dramatically due to blowing stellar wind. Bow shock occurs

                                                                                    Blast wave

                                                                                    field can be approximated as a lead shock wave, followed by a similar subsonic flow field. In simpler terms, a blast wave is an area of pressure expanding

                                                                                    Heliosphere

                                                                                    supersonic speeds within the Solar System. At the termination shock, a standing shock wave, the solar wind falls below the speed of sound and becomes subsonic

                                                                                    Atmospheric focusing

                                                                                    Atmospheric focusing is a type of wave interaction causing shock waves to affect areas at a greater distance than otherwise expected. Variations in the

                                                                                    Shocks and discontinuities (magnetohydrodynamics)

                                                                                    solar wind, behind astrophysical shock waves (supernova remnant) or due to the interaction of multiple CME driven shock waves. The Earth's magnetopause is

                                                                                    Particle image velocimetry

                                                                                    flows. Examples include the structure of a turbulent boundary layer/shock wave interaction, the vorticity of a cylinder wake or pitching airfoil, rod-airfoil

                                                                                    Corotating interaction region

                                                                                    greater distances from the Sun, these pressure waves can develop into shock waves. The three-dimensional structure of CIRs is influenced by the Sun's magnetic