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1Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment

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“Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment” Metadata:

  • Title: ➤  Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment
  • Author:
  • Language: English
  • Number of Pages: Median: 27
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - Langley Research Center
  • Publish Date:
  • Publish Location: Hampton, Va - [Springfield, Va

“Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment” 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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    2Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination

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    “Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination” Metadata:

    • Title: ➤  Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Washington, DC - Springfield, Va

    “Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination” 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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    Downloads Are Not Available:

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      3Development of multiobjective optimization techniques for sonic boom minimization

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      “Development of multiobjective optimization techniques for sonic boom minimization” Metadata:

      • Title: ➤  Development of multiobjective optimization techniques for sonic boom minimization
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - [Washington, D.C - [Washington, DC

      “Development of multiobjective optimization techniques for sonic boom minimization” 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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        4User's guide to PANCOR

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        “User's guide to PANCOR” Metadata:

        • Title: User's guide to PANCOR
        • Author:
        • Language: English
        • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - Hampton, Va

        “User's guide to PANCOR” 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

        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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          5Performance analysis of three dimensional integral equation computations on a massively parallel computer

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          “Performance analysis of three dimensional integral equation computations on a massively parallel computer” Metadata:

          • Title: ➤  Performance analysis of three dimensional integral equation computations on a massively parallel computer
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Washington, DC

          “Performance analysis of three dimensional integral equation computations on a massively parallel computer” 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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            6Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems

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            “Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems” Metadata:

            • Title: ➤  Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems
            • Author:
            • Language: English
            • Number of Pages: Median: 26
            • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
            • Publish Date:
            • Publish Location: ➤  Springfield, Va - [Washington, D.C.]

            “Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems” 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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              7Study of the mutual interaction between a wing wake and an encountering airplane

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              “Study of the mutual interaction between a wing wake and an encountering airplane” Metadata:

              • Title: ➤  Study of the mutual interaction between a wing wake and an encountering airplane
              • Author:
              • Language: English
              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
              • Publish Date:
              • Publish Location: ➤  Springfield, Va - [Washington, DC

              “Study of the mutual interaction between a wing wake and an encountering airplane” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1996
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

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                8Numerical approach for the aerodynamic analysis of airfoils with laminar separation

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                “Numerical approach for the aerodynamic analysis of airfoils with laminar separation” Metadata:

                • 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:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1985
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Access

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                  9Study of the integration of wind tunnel and computational methods for aerodynamic configurations

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                  “Study of the integration of wind tunnel and computational methods for aerodynamic configurations” Metadata:

                  • Title: ➤  Study of the integration of wind tunnel and computational methods for aerodynamic configurations
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 66
                  • 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

                  “Study of the integration of wind tunnel and computational methods for aerodynamic configurations” 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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                    10Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model

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                    “Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model” Metadata:

                    • Title: ➤  Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 108
                    • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
                    • Publish Date:
                    • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                    “Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model” 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

                    Downloads Are Not Available:

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                      11The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis

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                      “The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis” Metadata:

                      • Title: ➤  The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis
                      • Author:
                      • Number of Pages: Median: 23
                      • Publisher: ➤  Institute for Aerospace Studies
                      • Publish Date:
                      • Publish Location: [Downsview, Ont.]

                      “The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

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

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                      12Steady and unsteady three-dimensional transonic flow computations by integral equation method

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                      “Steady and unsteady three-dimensional transonic flow computations by integral equation method” Metadata:

                      • Title: ➤  Steady and unsteady three-dimensional transonic flow computations by integral equation method
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                      • Publish Date:
                      • Publish Location: ➤  Springfield, Va - [Washington, DC

                      “Steady and unsteady three-dimensional transonic flow computations by integral equation method” 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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                        13A numerical analysis applied to high angle of attack three-dimensional inlets

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

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

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

                        Edition Identifiers:

                        Access and General Info:

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

                        Online Access

                        Downloads Are Not Available:

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                          14USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics

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                          “USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics” Metadata:

                          • Title: ➤  USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 97
                          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
                          • Publish Date:
                          • Publish Location: [Washington, D.C.]

                          “USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics” 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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                          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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                            15A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies

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                            “A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies” Metadata:

                            • Title: ➤  A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies
                            • Author:
                            • Number of Pages: Median: 39
                            • Publisher: National Aerospace Laboratory
                            • Publish Date:
                            • Publish Location: Amsterdam

                            “A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1985
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

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                            16An approximate method for computing inviscid vortex wake roll-up. Part I: Theory and application

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                            “An approximate method for computing inviscid vortex wake roll-up. Part I: Theory and application” Metadata:

                            • Title: ➤  An approximate method for computing inviscid vortex wake roll-up. Part I: Theory and application
                            • Author:
                            • Number of Pages: Median: 80
                            • Publisher: National Aerospace Laboratory
                            • Publish Date:
                            • Publish Location: Amsterdam

                            “An approximate method for computing inviscid vortex wake roll-up. Part I: Theory and application” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1985
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

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