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1An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients

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“An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients” Metadata:

  • Title: ➤  An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients
  • Author:
  • Language: English
  • Publisher: ➤  Aerospace Engineering Dept., Texas A&M University, Texas Engineering Experiment Station - National Aeronautics and Space Administration - National Technical Information Service, distributor - Aerospace Engineering Dept., Texas A&M University - National Aeronautics and Space Administration]
  • Publish Date:
  • Publish Location: ➤  College Station, Tex - Springfield, Va - [Washington, D.C

“An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients” 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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    2Navier-Stokes calculations of transonic flows past cavities

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    “Navier-Stokes calculations of transonic flows past cavities” Metadata:

    • Title: ➤  Navier-Stokes calculations of transonic flows past cavities
    • Author:
    • Language: English
    • Publisher: ➤  Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division - Old Dominion University Research Foundation - For sale by the National Technical Information Service]
    • Publish Date:
    • Publish Location: ➤  Hampton, Va - Norfolk, Va - [Springfield, Va - [Washington, DC]

    “Navier-Stokes calculations of transonic flows past cavities” 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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      3An LU-SSOR scheme for the Euler and Navier-Stokes equations

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      “An LU-SSOR scheme for the Euler and Navier-Stokes equations” Metadata:

      • Title: ➤  An LU-SSOR scheme for the Euler and Navier-Stokes equations
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - New York, N. Y - [Washington, D.C.]

      “An LU-SSOR scheme for the Euler and Navier-Stokes equations” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

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

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        4Assessment of two-equation turbulence models for transonic flows

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        “Assessment of two-equation turbulence models for transonic flows” Metadata:

        • Title: ➤  Assessment of two-equation turbulence models for transonic flows
        • Author:
        • Language: English
        • Publisher: ➤  American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  Washington, D.C - Springfield, Va

        “Assessment of two-equation turbulence models for transonic flows” 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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          5Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems

          final report

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          “Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems” Metadata:

          • Title: ➤  Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - For sale by the National Technical Information Service
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Springfield, Va - [Washington, D.C.] - [Washington, DC

          “Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems” 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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            6Navier-Stokes computations on full wing-body configuration with oscillating control surfaces

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            “Navier-Stokes computations on full wing-body configuration with oscillating control surfaces” Metadata:

            • Title: ➤  Navier-Stokes computations on full wing-body configuration with oscillating control surfaces
            • Author:
            • Language: English
            • Publisher: ➤  [National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics
            • Publish Date:
            • Publish Location: ➤  Washington, DC - Springfield, Va

            “Navier-Stokes computations on full wing-body configuration with oscillating control surfaces” 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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              7Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wing

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              “Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wing” Metadata:

              • Title: ➤  Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wing
              • Author:
              • Language: English
              • Number of Pages: Median: 312
              • Publisher: ➤  For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
              • Publish Date:
              • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

              “Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wing” 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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                8A transonic-small-disturbance wing design methodology

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                “A transonic-small-disturbance wing design methodology” Metadata:

                • Title: ➤  A transonic-small-disturbance wing design methodology
                • Author:
                • Language: English
                • Number of Pages: Median: 28
                • Publisher: ➤  Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division - For sale by the National Technical Information Service]
                • Publish Date:
                • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

                “A transonic-small-disturbance wing design methodology” 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

                Online Access

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                  9Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design

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                  “Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design” Metadata:

                  • Title: ➤  Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 15
                  • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
                  • Publish Date:
                  • Publish Location: Hampton, Va - [Springfield, Va

                  “Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design” 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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                    10Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data

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                    “Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data” Metadata:

                    • Title: ➤  Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data
                    • 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

                    “Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

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

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                      11Full-potential modeling of blade-vortex interactions

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                      “Full-potential modeling of blade-vortex interactions” Metadata:

                      • Title: ➤  Full-potential modeling of blade-vortex interactions
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                      • Publish Date:
                      • Publish Location: [Springfield, Va - Hampton, Va

                      “Full-potential modeling of blade-vortex interactions” 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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                        12Transonic unsteady aerodynamics and aeroelasticity

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                        “Transonic unsteady aerodynamics and aeroelasticity” Metadata:

                        • Title: ➤  Transonic unsteady aerodynamics and aeroelasticity
                        • Author: ➤  
                        • Language: English
                        • Number of Pages: Median: 396
                        • Publisher: AGARD - Agard
                        • Publish Date:
                        • Publish Location: ➤  Neuilly sur Seine - Neuilly sur Seine, France

                        “Transonic unsteady aerodynamics and aeroelasticity” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

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

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                          13A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines

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                          “A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines” Metadata:

                          • Title: ➤  A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines
                          • 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

                          “A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines” 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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                          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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                            14The 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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                            15Nonlinear aspects of transonic aeroelasticity

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                            “Nonlinear aspects of transonic aeroelasticity” Metadata:

                            • Title: ➤  Nonlinear aspects of transonic aeroelasticity
                            • Author:
                            • Language: English
                            • Number of Pages: Median: 126
                            • Publisher: ➤  University of Toronto, Institute for Aerospace Studies - Institute for Aerospace Studies, University of Toronto
                            • Publish Date:
                            • Publish Location: ➤  [Downsview, Ont.] - [Toronto, Ont.]

                            “Nonlinear aspects of transonic aeroelasticity” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

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

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                            16A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel

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                            “A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel” Metadata:

                            • Title: ➤  A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel
                            • Author:
                            • Language: English
                            • Number of Pages: Median: 56
                            • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
                            • Publish Date:
                            • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                            “A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

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

                            Online Access

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

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                              17A direct-inverse method for transonic and separated flows about airfoils

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                              “A direct-inverse method for transonic and separated flows about airfoils” Metadata:

                              • Title: ➤  A direct-inverse method for transonic and separated flows about airfoils
                              • Author:
                              • Language: English
                              • Number of Pages: Median: 68
                              • Publisher: ➤  Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Office
                              • Publish Date:
                              • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

                              “A direct-inverse method for transonic and separated flows about airfoils” 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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                                18Transonic Navier-Stokes calculations about a 65⁰ delta wing

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                                “Transonic Navier-Stokes calculations about a 65⁰ delta wing” Metadata:

                                • Title: ➤  Transonic Navier-Stokes calculations about a 65⁰ delta wing
                                • 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

                                “Transonic Navier-Stokes calculations about a 65⁰ delta wing” 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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                                  19Finite difference calculation of an inviscid transonic flow over oscillating airfoils

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                                  “Finite difference calculation of an inviscid transonic flow over oscillating airfoils” Metadata:

                                  • Title: ➤  Finite difference calculation of an inviscid transonic flow over oscillating airfoils
                                  • Author:
                                  • Number of Pages: Median: 43
                                  • Publisher: Royal Aircraft Establishment
                                  • Publish Date:
                                  • Publish Location: Farnborough, Hants, England

                                  “Finite difference calculation of an inviscid transonic flow over oscillating airfoils” 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

                                  Online Access

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                                    20Application of viscous-inviscid interaction methods to transonic turbulent flows

                                    By

                                    “Application of viscous-inviscid interaction methods to transonic turbulent flows” Metadata:

                                    • Title: ➤  Application of viscous-inviscid interaction methods to transonic turbulent flows
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Technical Information Service, distributor - Engineering Research Institute - National Aeronautics and Space Administration - Iowa State University.
                                    • Publish Date:
                                    • Publish Location: ➤  [Washington, DC - [Ames, Iowa] - Springfield, Va

                                    “Application of viscous-inviscid interaction methods to transonic turbulent flows” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

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

                                    Online Access

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                                      21Multigrid calculation of three-dimensional turbomachinery flows

                                      By

                                      “Multigrid calculation of three-dimensional turbomachinery flows” Metadata:

                                      • Title: ➤  Multigrid calculation of three-dimensional turbomachinery flows
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University
                                      • Publish Date:
                                      • Publish Location: ➤  Ithaca, New York - [Washington, D.C.] - [Springfield, Va

                                      “Multigrid calculation of three-dimensional turbomachinery flows” 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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                                        22Extension of transonic flow computational concepts in the analysis of cavitated bearings

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                                        “Extension of transonic flow computational concepts in the analysis of cavitated bearings” Metadata:

                                        • Title: ➤  Extension of transonic flow computational concepts in the analysis of cavitated bearings
                                        • Author:
                                        • Language: English
                                        • Publisher: Lewis Research Center
                                        • Publish Date:
                                        • Publish Location: [Cleveland, Ohio

                                        “Extension of transonic flow computational concepts in the analysis of cavitated bearings” 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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                                          23An edge-based solution-adaptive method applied to the AIRPLANE code

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                                          “An edge-based solution-adaptive method applied to the AIRPLANE code” Metadata:

                                          • Title: ➤  An edge-based solution-adaptive method applied to the AIRPLANE code
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
                                          • Publish Date:
                                          • Publish Location: ➤  [Springfield, Va - [Moffett Field, CA]

                                          “An edge-based solution-adaptive method applied to the AIRPLANE code” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

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

                                          Online Access

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

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                                            24Grid studies for thin-layer Navier-Stokes computations of airfoil flowfields

                                            By

                                            “Grid studies for thin-layer Navier-Stokes computations of airfoil flowfields” Metadata:

                                            • Title: ➤  Grid studies for thin-layer Navier-Stokes computations of airfoil flowfields
                                            • Author:
                                            • Number of Pages: Median: 1288
                                            • Publisher: ➤  Sine nomine - American Institute of Aeronautics and Astronautics
                                            • Publish Date:
                                            • Publish Location: [S.l.] - Washington, D. C

                                            “Grid studies for thin-layer Navier-Stokes computations of airfoil flowfields” Subjects and Themes:

                                            Edition Identifiers:

                                            Access and General Info:

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

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                                            25Blockage development in a transonic, axial compressor rotor

                                            By

                                            “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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                                              26Aerodynamics of engine-airframe interaction

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                                              “Aerodynamics of engine-airframe interaction” Metadata:

                                              • Title: ➤  Aerodynamics of engine-airframe interaction
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                              • Publish Date:
                                              • Publish Location: ➤  Springfield, Va - [Washington, DC

                                              “Aerodynamics of engine-airframe interaction” Subjects and Themes:

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                                              Access and General Info:

                                              • First Year Published: 1988
                                              • Is Full Text Available: No
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                                                27Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method

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                                                “Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Metadata:

                                                • Title: ➤  Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
                                                • 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

                                                “Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Subjects and Themes:

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                                                • First Year Published: 1996
                                                • Is Full Text Available: No
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                                                  28Development of direct-inverse 3-D methods for applied aerodynamic design and analysis

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                                                  “Development of direct-inverse 3-D methods for applied aerodynamic design and analysis” Metadata:

                                                  • Title: ➤  Development of direct-inverse 3-D methods for applied aerodynamic design and analysis
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University
                                                  • Publish Date:
                                                  • Publish Location: ➤  College Station, Tex - Springfield, Va - [Washington, DC

                                                  “Development of direct-inverse 3-D methods for applied aerodynamic design and analysis” Subjects and Themes:

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                                                  • First Year Published: 1988
                                                  • Is Full Text Available: No
                                                  • Is The Book Public: No
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                                                    29On approximate factorization schemes for solving the full potential equation

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                                                    “On approximate factorization schemes for solving the full potential equation” Metadata:

                                                    • Title: ➤  On approximate factorization schemes for solving the full potential equation
                                                    • Author:
                                                    • Language: English
                                                    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                    • Publish Date:
                                                    • Publish Location: ➤  [Springfield, Va - Washington, DC

                                                    “On approximate factorization schemes for solving the full potential equation” Subjects and Themes:

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                                                    • First Year Published: 1997
                                                    • Is Full Text Available: No
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                                                      30Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method

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                                                      “Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Metadata:

                                                      • Title: ➤  Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
                                                      • Author: ➤  
                                                      • Language: English
                                                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                      • Publish Date:
                                                      • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                      “Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Subjects and Themes:

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                                                      • First Year Published: 1996
                                                      • Is Full Text Available: No
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                                                        31Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers

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                                                        “Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers” Metadata:

                                                        • Title: ➤  Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers
                                                        • Author:
                                                        • Language: English
                                                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                        • Publish Date:
                                                        • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                                        “Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers” Subjects and Themes:

                                                        Edition Identifiers:

                                                        Access and General Info:

                                                        • First Year Published: 1995
                                                        • Is Full Text Available: No
                                                        • Is The Book Public: No
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                                                          32A vapor generator for transonic flow visualization

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                                                          “A vapor generator for transonic flow visualization” Metadata:

                                                          • Title: ➤  A vapor generator for transonic flow visualization
                                                          • Author:
                                                          • Language: English
                                                          • Number of Pages: Median: 17
                                                          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                                                          • Publish Date:
                                                          • Publish Location: Hampton, Va

                                                          “A vapor generator for transonic flow visualization” Subjects and Themes:

                                                          Edition Identifiers:

                                                          Access and General Info:

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

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                                                            33External boundary conditions for three-dimensional problems of computational aerodynamics

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

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

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

                                                            Edition Identifiers:

                                                            Access and General Info:

                                                            • First Year Published: 1997
                                                            • Is Full Text Available: No
                                                            • Is The Book Public: No
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                                                              34Numerical simulation of 2-D unsteady transonic flows using the full-potential equation

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                                                              “Numerical simulation of 2-D unsteady transonic flows using the full-potential equation” Metadata:

                                                              • Title: ➤  Numerical simulation of 2-D unsteady transonic flows using the full-potential equation
                                                              • Author:
                                                              • Number of Pages: Median: 12
                                                              • Publisher: AIAA
                                                              • Publish Date:
                                                              • Publish Location: New York

                                                              “Numerical simulation of 2-D unsteady transonic flows using the full-potential equation” Subjects and Themes:

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                                                              • First Year Published: 1983
                                                              • Is Full Text Available: No
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                                                              35Multigrid methods for aerodynamic problems in complex geometries

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

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

                                                              “Multigrid methods for aerodynamic problems in complex geometries” Subjects and Themes:

                                                              Edition Identifiers:

                                                              Access and General Info:

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

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                                                                36Wind tunnel wall interference

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                                                                “Wind tunnel wall interference” Metadata:

                                                                • Title: Wind tunnel wall interference
                                                                • Author:
                                                                • Number of Pages: Median: 15
                                                                • Publisher: ➤  Air Force Office of Scientific Research
                                                                • Publish Date:
                                                                • Publish Location: Bolling Air Force Base, D.C

                                                                “Wind tunnel wall interference” 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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                                                                37SIMPROP

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                                                                “SIMPROP” Metadata:

                                                                • Title: SIMPROP
                                                                • Author:
                                                                • Number of Pages: Median: 43
                                                                • Publisher: National Aerospace Laboratory
                                                                • Publish Date:
                                                                • Publish Location: Amsterdam

                                                                “SIMPROP” 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

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                                                                38A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation

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                                                                “A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation” Metadata:

                                                                • Title: ➤  A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation
                                                                • Author:
                                                                • Number of Pages: Median: 79
                                                                • Publisher: Langley Research Center
                                                                • Publish Date:
                                                                • Publish Location: Hampton, Va

                                                                “A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1987
                                                                • Is Full Text Available: No
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                                                                39Experimentelle Untersuchung der Ausbreitung strossinduzierter Storungen an transsonischen Profilen

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                                                                “Experimentelle Untersuchung der Ausbreitung strossinduzierter Storungen an transsonischen Profilen” Metadata:

                                                                • Title: ➤  Experimentelle Untersuchung der Ausbreitung strossinduzierter Storungen an transsonischen Profilen
                                                                • Author:
                                                                • Number of Pages: Median: 123
                                                                • Publisher: DFVLR
                                                                • Publish Date:
                                                                • Publish Location: Koln

                                                                “Experimentelle Untersuchung der Ausbreitung strossinduzierter Storungen an transsonischen Profilen” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1987
                                                                • Is Full Text Available: No
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                                                                40Numerical simulation of two-dimensional transonic flow over thin oscillating airfoil

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                                                                “Numerical simulation of two-dimensional transonic flow over thin oscillating airfoil” Metadata:

                                                                • Title: ➤  Numerical simulation of two-dimensional transonic flow over thin oscillating airfoil
                                                                • Author:
                                                                • Number of Pages: Median: 11
                                                                • Publisher: ➤  Information Centre for Aeronautics
                                                                • Publish Date:
                                                                • Publish Location: Praha, Czechoslovakia

                                                                “Numerical simulation of two-dimensional transonic flow over thin oscillating airfoil” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1986
                                                                • Is Full Text Available: No
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                                                                41Development and application of adaptive grids in two-dimensional transonic calculations

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                                                                “Development and application of adaptive grids in two-dimensional transonic calculations” Metadata:

                                                                • Title: ➤  Development and application of adaptive grids in two-dimensional transonic calculations
                                                                • Author:
                                                                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                                                                • Publish Date:
                                                                • Publish Location: New York

                                                                “Development and application of adaptive grids in two-dimensional transonic calculations” 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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                                                                42Numerical calculation of unsteady inviscid rotational transonic flow past airfoils using Euler equations

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                                                                “Numerical calculation of unsteady inviscid rotational transonic flow past airfoils using Euler equations” Metadata:

                                                                • Title: ➤  Numerical calculation of unsteady inviscid rotational transonic flow past airfoils using Euler equations
                                                                • Author:
                                                                • Number of Pages: Median: 262
                                                                • Publisher: Cornell University
                                                                • Publish Date:
                                                                • Publish Location: [Ithaca, N.Y.?]

                                                                “Numerical calculation of unsteady inviscid rotational transonic flow past airfoils using Euler equations” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1987
                                                                • Is Full Text Available: No
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                                                                43Revised results of the unsteady transonic pressure measurements on the LANN model

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                                                                “Revised results of the unsteady transonic pressure measurements on the LANN model” Metadata:

                                                                • Title: ➤  Revised results of the unsteady transonic pressure measurements on the LANN model
                                                                • Author:
                                                                • Number of Pages: Median: 156
                                                                • Publisher: National Aerospace Laboratory
                                                                • Publish Date:
                                                                • Publish Location: Amsterdam

                                                                “Revised results of the unsteady transonic pressure measurements on the LANN model” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1989
                                                                • Is Full Text Available: No
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                                                                44Unsteady transonic flows past airfoils using the Euler equations

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                                                                “Unsteady transonic flows past airfoils using the Euler equations” Metadata:

                                                                • Title: ➤  Unsteady transonic flows past airfoils using the Euler equations
                                                                • Author:
                                                                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                                                                • Publish Date:
                                                                • Publish Location: New York

                                                                “Unsteady transonic flows past airfoils using the Euler equations” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1986
                                                                • Is Full Text Available: No
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                                                                45Transonic flow around airfoils with relaxation and energy supply by homogeneous condensation

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                                                                “Transonic flow around airfoils with relaxation and energy supply by homogeneous condensation” Metadata:

                                                                • Title: ➤  Transonic flow around airfoils with relaxation and energy supply by homogeneous condensation
                                                                • Author:
                                                                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                                                                • Publish Date:
                                                                • Publish Location: New York

                                                                “Transonic flow around airfoils with relaxation and energy supply by homogeneous condensation” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1989
                                                                • Is Full Text Available: No
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                                                                46Large-scale numerical aerodynamic simulations for complete aircraft configurations

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                                                                “Large-scale numerical aerodynamic simulations for complete aircraft configurations” Metadata:

                                                                • Title: ➤  Large-scale numerical aerodynamic simulations for complete aircraft configurations
                                                                • Author:
                                                                • Number of Pages: Median: 12
                                                                • Publisher: National Aerospace Laboratory
                                                                • Publish Date:
                                                                • Publish Location: Tokyo, Japan

                                                                “Large-scale numerical aerodynamic simulations for complete aircraft configurations” 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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                                                                47Wave drag determination in the transonic full-potential flow code matrics

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                                                                “Wave drag determination in the transonic full-potential flow code matrics” Metadata:

                                                                • Title: ➤  Wave drag determination in the transonic full-potential flow code matrics
                                                                • Author:
                                                                • Number of Pages: Median: 29
                                                                • Publisher: National Aerospace Laboratory
                                                                • Publish Date:
                                                                • Publish Location: Amsterdam

                                                                “Wave drag determination in the transonic full-potential flow code matrics” 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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                                                                48Computation of unsteady transonic flows over moving airfoils

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                                                                “Computation of unsteady transonic flows over moving airfoils” Metadata:

                                                                • Title: ➤  Computation of unsteady transonic flows over moving airfoils
                                                                • Author:
                                                                • Number of Pages: Median: 146
                                                                • Publisher: Princeton University
                                                                • Publish Date:
                                                                • Publish Location: Princeton, N.J

                                                                “Computation of unsteady transonic flows over moving airfoils” 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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                                                                49Three-dimensional Euler equation simulation of propeller-wing interaction in transonic flow

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                                                                “Three-dimensional Euler equation simulation of propeller-wing interaction in transonic flow” Metadata:

                                                                • Title: ➤  Three-dimensional Euler equation simulation of propeller-wing interaction in transonic flow
                                                                • Author:
                                                                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                                                                • Publish Date:
                                                                • Publish Location: New York

                                                                “Three-dimensional Euler equation simulation of propeller-wing interaction in transonic flow” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1983
                                                                • Is Full Text Available: No
                                                                • Is The Book Public: No
                                                                • Access Status: No_ebook

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                                                                50Modifications to the inlet flow field of a transonic compressor rotor

                                                                By

                                                                Book's cover

                                                                “Modifications to the inlet flow field of a transonic compressor rotor” Metadata:

                                                                • Title: ➤  Modifications to the inlet flow field of a transonic compressor rotor
                                                                • Author:
                                                                • Language: English
                                                                • Number of Pages: Median: 44
                                                                • Publisher: ➤  Available from National Technical Information Service - Naval Postgraduate School
                                                                • Publish Date:
                                                                • Publish Location: ➤  Springfield, Va - Monterey, Calif

                                                                “Modifications to the inlet flow field of a transonic compressor rotor” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1985
                                                                • Is Full Text Available: Yes
                                                                • Is The Book Public: Yes
                                                                • Access Status: Public

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