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1Boundary layers

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“Boundary layers” Metadata:

  • Title: Boundary layers
  • Author:
  • Language: English
  • Number of Pages: Median: 269
  • Publisher: ➤  Boston - American Institute of Aeronautics and Astronautics - BSP - BSP Professional Books - Brand: Amer Inst of Aeronautics - Amer Inst of Aeronautics &
  • Publish Date:
  • Publish Location: Washington, DC - Oxford

“Boundary layers” Subjects and Themes:

Edition Identifiers:

Access and General Info:

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

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    2The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil

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    “The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Metadata:

    • Title: ➤  The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
    • Author:
    • Language: English
    • Number of Pages: Median: 18
    • Publisher: ➤  Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - For sale by the National Technical Information Service
    • Publish Date:
    • Publish Location: ➤  [Washington, D.C.] - Springfield, Va - Hampton, Va

    “The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

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

    Online Access

    Downloads Are Not Available:

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      3Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment

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      “Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment” Metadata:

      • Title: ➤  Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment
      • Author:
      • Language: English
      • Number of Pages: Median: 48
      • Publisher: ➤  NASA Center for AeroSpace Information [distributor] - National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service [distributor - Available from NASA Center for AeroSpace Information
      • Publish Date:
      • Publish Location: ➤  Springfield, VA - Edwards, Calif - Hanover, Md - Hanover, MD

      “Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment” 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

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        4Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research

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        “Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research” Metadata:

        • Title: ➤  Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Washington, DC - Springfield, Va

        “Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

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

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          5The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil

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          “The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Metadata:

          • Title: ➤  The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
          • Author:
          • Number of Pages: Median: 120
          • Publisher: Langley Research Center
          • Publish Date:
          • Publish Location: Hampton, Va

          “The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

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

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          6Non-linear boundary-layer receptivity due to distributed surface roughness

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          “Non-linear boundary-layer receptivity due to distributed surface roughness” Metadata:

          • Title: ➤  Non-linear boundary-layer receptivity due to distributed surface roughness
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - Old Dominion University Research Foundation, Dept. of Mechanical Engineering, College of Engineering & Technology - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  [Washington, D.C - Norfolk, Va - Springfield, Va

          “Non-linear boundary-layer receptivity due to distributed surface roughness” 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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            7Supersonic laminar flow control research

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            “Supersonic laminar flow control research” Metadata:

            • Title: ➤  Supersonic laminar flow control research
            • Author:
            • Language: English
            • Publisher: ➤  Ames Research Center - National Aeronautics and Space Administration - University of Tennessee, Space Institute - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  Tullahoma, TN - [Springfield, Va - Moffett Field, CA - [Washington, DC - Springfield, Va

            “Supersonic laminar flow control research” 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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              8A review of high-speed, convective, heat-transfer computation methods

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              “A review of high-speed, convective, heat-transfer computation methods” Metadata:

              • Title: ➤  A review of high-speed, convective, heat-transfer computation methods
              • Author:
              • Language: English
              • Number of Pages: Median: 33
              • Publisher: ➤  Ames Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
              • Publish Date:
              • Publish Location: ➤  Moffett Field, Calif - [Washington, D.C.]

              “A review of high-speed, convective, heat-transfer computation methods” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

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

              Online Access

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                9Instability and transition of flow at, and near, an attachment-line

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                “Instability and transition of flow at, and near, an attachment-line” Metadata:

                • Title: ➤  Instability and transition of flow at, and near, an attachment-line
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Aeronautics and Space Administration - National Technical Information Service, distributor
                • Publish Date:
                • Publish Location: ➤  Hampton, Va - [Washington, DC - [Springfield, Va - Springfield, Va

                “Instability and transition of flow at, and near, an attachment-line” 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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                  10Theoretical and experimental investigations of incompressible laminar boundary layers with and without suction

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                  “Theoretical and experimental investigations of incompressible laminar boundary layers with and without suction” Metadata:

                  • Title: ➤  Theoretical and experimental investigations of incompressible laminar boundary layers with and without suction
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 245
                  • Publisher: ➤  Technische Wetenschappen aan de^Technische Hogeschool to Delft - Sine nomine
                  • Publish Date:
                  • Publish Location: Delft - [s.l.]

                  “Theoretical and experimental investigations of incompressible laminar boundary layers with and without suction” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

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

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                  11Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel

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                  “Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel” Metadata:

                  • Title: ➤  Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                  • Publish Date:
                  • Publish Location: ➤  Springfield, Va - [Washington, D.C

                  “Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel” 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:

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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:

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                      13Numerische Simulation der Wechselwirkung von Druckwellen mit laminaren und turbulenten Grenzschichten

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                      “Numerische Simulation der Wechselwirkung von Druckwellen mit laminaren und turbulenten Grenzschichten” Metadata:

                      • Title: ➤  Numerische Simulation der Wechselwirkung von Druckwellen mit laminaren und turbulenten Grenzschichten
                      • Author:
                      • Language: ger
                      • Number of Pages: Median: 102
                      • Publisher: DFVLR
                      • Publish Date:
                      • Publish Location: Koln - Köln

                      “Numerische Simulation der Wechselwirkung von Druckwellen mit laminaren und turbulenten Grenzschichten” 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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                      14Validation 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:

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                        15The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity

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                        “The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity” Metadata:

                        • Title: ➤  The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity
                        • Author:
                        • Language: English
                        • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering
                        • Publish Date:
                        • Publish Location: Hampton, Va - [Springfield, Va

                        “The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

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

                        Online Access

                        Downloads Are Not Available:

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                          16The interactions of a flame and its self-induced boundary layer

                          By

                          “The interactions of a flame and its self-induced boundary layer” Metadata:

                          • Title: ➤  The interactions of a flame and its self-induced boundary layer
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
                          • Publish Date:
                          • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

                          “The interactions of a flame and its self-induced boundary layer” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

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

                          Online Access

                          Downloads Are Not Available:

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

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                            17Heat transfer in a laminar boundary layer at Mach 2.5 from a surface having a temperature distribution

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                            “Heat transfer in a laminar boundary layer at Mach 2.5 from a surface having a temperature distribution” Metadata:

                            • Title: ➤  Heat transfer in a laminar boundary layer at Mach 2.5 from a surface having a temperature distribution
                            • Author:
                            • Number of Pages: Median: 19
                            • Publisher: ➤  [Institue of Aerophysics] - Institute of Aerophysics
                            • Publish Date:
                            • Publish Location: [Downsview, Ont.]

                            “Heat transfer in a laminar boundary layer at Mach 2.5 from a surface having a temperature distribution” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1957
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

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                            18Quantitative laser Schlieren measurements in an expanding hypersonic laminar boundary layer

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                            “Quantitative laser Schlieren measurements in an expanding hypersonic laminar boundary layer” Metadata:

                            • Title: ➤  Quantitative laser Schlieren measurements in an expanding hypersonic laminar boundary layer
                            • Author:
                            • Publisher: ➤  [Institute for Aerospace Studies] - Institute for Aerospace Studies
                            • Publish Date:
                            • Publish Location: [Downsview, Ont.]

                            “Quantitative laser Schlieren measurements in an expanding hypersonic laminar boundary layer” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1971
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

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                            19Acoustic excitation of Tollmien-Schlichting waves in a laminar boundary layer

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                            “Acoustic excitation of Tollmien-Schlichting waves in a laminar boundary layer” Metadata:

                            • Title: ➤  Acoustic excitation of Tollmien-Schlichting waves in a laminar boundary layer
                            • Author:
                            • Publisher: ➤  [Institute for Aerospace Studies] - Institute for Aerospace Studies
                            • Publish Date:
                            • Publish Location: [Downsview, Ont.]

                            “Acoustic excitation of Tollmien-Schlichting waves in a laminar boundary layer” 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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                            20Effects of probe size on measurements in a laminar boundary layer in supersonic flow

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                            “Effects of probe size on measurements in a laminar boundary layer in supersonic flow” Metadata:

                            • Title: ➤  Effects of probe size on measurements in a laminar boundary layer in supersonic flow
                            • Author:
                            • Publisher: ➤  Institute of Aerophysics - Dept. of Aeronautical Engineering and Aerophysics
                            • Publish Date:
                            • Publish Location: [Downsview, Ont.]

                            “Effects of probe size on measurements in a laminar boundary layer in supersonic flow” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1956
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

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                            21Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions

                            By

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

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

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

                            Edition Identifiers:

                            Access and General Info:

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

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                            22Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions

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                            “Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions” Metadata:

                            • Title: ➤  Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions
                            • 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

                            “Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions” 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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                              23Laminar-boundary-layer oscillations and transition on a flat plate

                              By

                              “Laminar-boundary-layer oscillations and transition on a flat plate” Metadata:

                              • Title: ➤  Laminar-boundary-layer oscillations and transition on a flat plate
                              • Author:
                              • Number of Pages: Median: 71
                              • Publisher: ➤  National Advisory Committee for Aeronautics
                              • Publish Date:
                              • Publish Location: [Washington?]

                              “Laminar-boundary-layer oscillations and transition on a flat plate” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1942
                              • Is Full Text Available: No
                              • Is The Book Public: No
                              • Access Status: No_ebook

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                              24Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point

                              By

                              “Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point” Metadata:

                              • Title: ➤  Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                              • Publish Date:
                              • Publish Location: ➤  [Springfield, Va - Washington, D.C

                              “Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

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

                              Online 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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                                25Stability of the laminar boundary layer in a streamwise corner

                                By

                                “Stability of the laminar boundary layer in a streamwise corner” Metadata:

                                • Title: ➤  Stability of the laminar boundary layer in a streamwise corner
                                • Author:
                                • Language: English
                                • Publisher: ➤  Old Dominion University Research Foundation - National Aeronautics and Space Administration, Langley Research Center
                                • Publish Date:
                                • Publish Location: Norfolk, Va - Hampton, Va

                                “Stability of the laminar boundary layer in a streamwise corner” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

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

                                Online Access

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                                  26Practical calculation of laminar and turbulent bled-off boundary layers

                                  By

                                  “Practical calculation of laminar and turbulent bled-off boundary layers” Metadata:

                                  • Title: ➤  Practical calculation of laminar and turbulent bled-off boundary layers
                                  • Author:
                                  • Number of Pages: Median: 57
                                  • Publisher: NASA
                                  • Publish Date:
                                  • Publish Location: Washington, D. C

                                  “Practical calculation of laminar and turbulent bled-off boundary layers” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

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

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                                  27Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment

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                                  • Title: ➤  Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment
                                  • Author:
                                  • Number of Pages: Median: 120
                                  • Publisher: Langley Research Center
                                  • Publish Date:
                                  • Publish Location: Hampton, Va

                                  “Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment” Subjects and Themes:

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                                  28The response of the unsteady laminar boundary layer to leading edge acoustic diffraction

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                                  • Title: ➤  The response of the unsteady laminar boundary layer to leading edge acoustic diffraction
                                  • Author:
                                  • Number of Pages: Median: 62
                                  • Publisher: ➤  Department of Aerospace Science and Engineering
                                  • Publish Date:
                                  • Publish Location: [Downsview, Ont.]

                                  “The response of the unsteady laminar boundary layer to leading edge acoustic diffraction” Subjects and Themes:

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                                  29Analysis and evaluation of an integrated laminar flow control propulsion system

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                                  • Title: ➤  Analysis and evaluation of an integrated laminar flow control propulsion system
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                  • Publish Date:
                                  • Publish Location: ➤  Springfield, Va - [Washington, DC

                                  “Analysis and evaluation of an integrated laminar flow control propulsion system” Subjects and Themes:

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                                  • First Year Published: 1993
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                                    30Some characteristics of bypass transition in a heated boundary layer

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                                    • Title: ➤  Some characteristics of bypass transition in a heated boundary layer
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                    • Publish Date:
                                    • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                    “Some characteristics of bypass transition in a heated boundary layer” Subjects and Themes:

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                                    • First Year Published: 1989
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                                      31Some characteristics of bypass transition in a heated boundary layer

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                                      • Title: ➤  Some characteristics of bypass transition in a heated boundary layer
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                      • Publish Date:
                                      • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                      “Some characteristics of bypass transition in a heated boundary layer” Subjects and Themes:

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                                        32Parametric study on laminar flow for finite wings at supersonic speeds

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                                        • Title: ➤  Parametric study on laminar flow for finite wings at supersonic speeds
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                        • Publish Date:
                                        • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                        “Parametric study on laminar flow for finite wings at supersonic speeds” Subjects and Themes:

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                                        • First Year Published: 1994
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                                          33Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia

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                                          • Title: ➤  Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  Dept. of Mechanical and Aerospace Engineering, Arizona State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
                                          • Publish Date:
                                          • Publish Location: ➤  Springfield, Va - Tempe, Ariz - [Washington, DC

                                          “Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia” Subjects and Themes:

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                                          • First Year Published: 1988
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                                            34Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers

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                                            • Title: ➤  Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers
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                                            • Language: English
                                            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                                            • Publish Date:
                                            • Publish Location: [Springfield, Va - Hampton, Va

                                            “Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers” Subjects and Themes:

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                                            • First Year Published: 1995
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                                              35Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers

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                                              • Title: ➤  Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers
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                                              • Language: English
                                              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                              • Publish Date:
                                              • Publish Location: Hampton, Va - [Springfield, Va

                                              “Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers” Subjects and Themes:

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                                                36Numerical approach for the aerodynamic analysis of airfoils with laminar separation

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                                                • Title: ➤  Numerical approach for the aerodynamic analysis of airfoils with laminar separation
                                                • Author:
                                                • Language: English
                                                • Publisher: ➤  McDonnel Douglas Corporation, McDonnel Aircraft Company - National Aeronautics and Space Administration, Langley Research Center
                                                • Publish Date:
                                                • Publish Location: St. Louis, Mo - Hampton, Va

                                                “Numerical approach for the aerodynamic analysis of airfoils with laminar separation” Subjects and Themes:

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                                                • First Year Published: 1985
                                                • Is Full Text Available: No
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                                                  37Structural tests and development of a laminar flow control wing surface composite chordwise joint

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                                                  “Structural tests and development of a laminar flow control wing surface composite chordwise joint” Metadata:

                                                  • Title: ➤  Structural tests and development of a laminar flow control wing surface composite chordwise joint
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Lockheed-Georgia Company
                                                  • Publish Date:
                                                  • Publish Location: Hampton, Va - Marietta, Ga

                                                  “Structural tests and development of a laminar flow control wing surface composite chordwise joint” Subjects and Themes:

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                                                  • First Year Published: 1984
                                                  • Is Full Text Available: No
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                                                    38Engineering correlations of variable-property effects on laminar forced convection mass transfer for dilute vapor species and small particles in air

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                                                    “Engineering correlations of variable-property effects on laminar forced convection mass transfer for dilute vapor species and small particles in air” Metadata:

                                                    • Title: ➤  Engineering correlations of variable-property effects on laminar forced convection mass transfer for dilute vapor species and small particles in air
                                                    • Author:
                                                    • Language: English
                                                    • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
                                                    • Publish Date:
                                                    • Publish Location: [Cleveland, Ohio]

                                                    “Engineering correlations of variable-property effects on laminar forced convection mass transfer for dilute vapor species and small particles in air” Subjects and Themes:

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                                                    • First Year Published: 1984
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                                                      39Simulation of glancing shock wave and boundary layer interaction

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                                                      • Title: ➤  Simulation of glancing shock wave and boundary layer interaction
                                                      • Author:
                                                      • Language: English
                                                      • Number of Pages: Median: 10
                                                      • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
                                                      • Publish Date:
                                                      • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

                                                      “Simulation of glancing shock wave and boundary layer interaction” Subjects and Themes:

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                                                      • First Year Published: 1989
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                                                      40Simulation of glancing shock wave and boundary layer interaction

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                                                      • Title: ➤  Simulation of glancing shock wave and boundary layer interaction
                                                      • Author:
                                                      • Language: English
                                                      • Number of Pages: Median: 10
                                                      • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
                                                      • Publish Date:
                                                      • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

                                                      “Simulation of glancing shock wave and boundary layer interaction” Subjects and Themes:

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                                                      • First Year Published: 1989
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                                                        41Compressible laminar boundary layers for perfect and real gases in equilibrium at Mach numbers to 30

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                                                        “Compressible laminar boundary layers for perfect and real gases in equilibrium at Mach numbers to 30” Metadata:

                                                        • Title: ➤  Compressible laminar boundary layers for perfect and real gases in equilibrium at Mach numbers to 30
                                                        • Author:
                                                        • Number of Pages: Median: 13
                                                        • Publisher: ➤  American Institute of Aeronautics and Astronautics
                                                        • Publish Date:
                                                        • Publish Location: Washington, D. C

                                                        “Compressible laminar boundary layers for perfect and real gases in equilibrium at Mach numbers to 30” Subjects and Themes:

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                                                        • First Year Published: 1992
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                                                        42Calculation of laminar boundary layer flow on rotating blades

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                                                        • Title: ➤  Calculation of laminar boundary layer flow on rotating blades
                                                        • Author:
                                                        • Publisher: Cornell University
                                                        • Publish Date:
                                                        • Publish Location: [Ithaca, N.Y.]

                                                        “Calculation of laminar boundary layer flow on rotating blades” Subjects and Themes:

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                                                        43Textbook multigrid efficiency for the incompressible Navier-Stokes equations

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                                                        • Title: ➤  Textbook multigrid efficiency for the incompressible Navier-Stokes equations
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                                                        • 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

                                                        “Textbook multigrid efficiency for the incompressible Navier-Stokes equations” Subjects and Themes:

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                                                        • First Year Published: 1999
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                                                          44Flight demonstration of a shock location sensor using constant voltage hot-film anemometry

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                                                          • Title: ➤  Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                                                          • Publish Date:
                                                          • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                                          “Flight demonstration of a shock location sensor using constant voltage hot-film anemometry” Subjects and Themes:

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                                                          • First Year Published: 1997
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                                                            45Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5

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                                                            • Title: ➤  Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5
                                                            • Author:
                                                            • Number of Pages: Median: 58
                                                            • Publisher: Langley Research Center
                                                            • Publish Date:
                                                            • Publish Location: Hampton, Va

                                                            “Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5” Subjects and Themes:

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                                                            • First Year Published: 1986
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                                                            46User's manual for the Langley boundary layer noise propagation program (MRS-BLP)

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                                                            • Title: ➤  User's manual for the Langley boundary layer noise propagation program (MRS-BLP)
                                                            • 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

                                                            “User's manual for the Langley boundary layer noise propagation program (MRS-BLP)” Subjects and Themes:

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                                                            • First Year Published: 1991
                                                            • Is Full Text Available: No
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                                                              47Overview of laminar flow control

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                                                              “Overview of laminar flow control” Metadata:

                                                              • Title: ➤  Overview of laminar flow control
                                                              • 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

                                                              “Overview of laminar flow control” Subjects and Themes:

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                                                              • First Year Published: 1998
                                                              • Is Full Text Available: No
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                                                                48Investigation of an oblique shock wave/laminar boundary layer interaction using LDV

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                                                                “Investigation of an oblique shock wave/laminar boundary layer interaction using LDV” Metadata:

                                                                • Title: ➤  Investigation of an oblique shock wave/laminar boundary layer interaction using LDV
                                                                • Author:
                                                                • Number of Pages: Median: 29
                                                                • Publisher: ➤  von Karman Institute for Fluid Dynamics
                                                                • Publish Date:
                                                                • Publish Location: Rhode Saint Genese, Belgium

                                                                “Investigation of an oblique shock wave/laminar boundary layer interaction using LDV” Subjects and Themes:

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                                                                • First Year Published: 1984
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                                                                49Untersuchung kunstlich angeregter Instabilitaten in einer zweidimensionalen laminaren Grenzschichtstromung mit Hilfe der Particle Image Velocimetry

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                                                                • Title: ➤  Untersuchung kunstlich angeregter Instabilitaten in einer zweidimensionalen laminaren Grenzschichtstromung mit Hilfe der Particle Image Velocimetry
                                                                • Author:
                                                                • Number of Pages: Median: 91
                                                                • Publisher: DLR
                                                                • Publish Date:
                                                                • Publish Location: Koln, Germany

                                                                “Untersuchung kunstlich angeregter Instabilitaten in einer zweidimensionalen laminaren Grenzschichtstromung mit Hilfe der Particle Image Velocimetry” Subjects and Themes:

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                                                                • First Year Published: 1993
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                                                                50Nonsimilar solution of the laminar boundary layer in an oscillatory flow by an integral matrix method

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                                                                • Title: ➤  Nonsimilar solution of the laminar boundary layer in an oscillatory flow by an integral matrix method
                                                                • Author:
                                                                • Language: English
                                                                • Number of Pages: Median: 100
                                                                • Publisher: Naval Postgraduate School
                                                                • Publish Date:
                                                                • Publish Location: Monterey, California

                                                                “Nonsimilar solution of the laminar boundary layer in an oscillatory flow by an integral matrix method” Subjects and Themes:

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                                                                • First Year Published: 1969
                                                                • Is Full Text Available: Yes
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