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Source: The Open Library

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1A near-wall Reynolds-stress closure without wall normals

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“A near-wall Reynolds-stress closure without wall normals” Metadata:

  • Title: ➤  A near-wall Reynolds-stress closure without wall normals
  • Author:
  • Language: English
  • Number of Pages: Median: 263
  • Publisher: ➤  College of Engineering and Applied Sciences, Arizona State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Washington, DC - Tempe, Ariz - Springfield, Va

“A near-wall Reynolds-stress closure without wall normals” 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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    2Aerodynamics of low reynolds number flyers

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    Book's cover

    “Aerodynamics of low reynolds number flyers” Metadata:

    • Title: ➤  Aerodynamics of low reynolds number flyers
    • Author:
    • Language: English
    • Number of Pages: Median: 196
    • Publisher: Cambridge University Press
    • Publish Date:
    • Publish Location: Cambridge - New York

    “Aerodynamics of low reynolds number flyers” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 2007
    • Is Full Text Available: Yes
    • Is The Book Public: No
    • Access Status: Printdisabled

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      3Hot-jet simulation in cryogenic wind tunnels

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      “Hot-jet simulation in cryogenic wind tunnels” Metadata:

      • Title: ➤  Hot-jet simulation in cryogenic wind tunnels
      • Author:
      • Language: English
      • Number of Pages: Median: 45
      • Publisher: ➤  For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and SpaceAdministration - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
      • Publish Date:
      • Publish Location: ➤  Washington D.C - Hampton, Va - Washington, D.C - [Springfield, Va - [Washington, DC]

      “Hot-jet simulation in cryogenic wind tunnels” 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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        4Assessment of dual-point drag reduction for an executive-jet modified airfoil section

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        “Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Metadata:

        • Title: ➤  Assessment of dual-point drag reduction for an executive-jet modified airfoil section
        • Author:
        • Language: English
        • Number of Pages: Median: 114
        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from National Technical Information Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langly Research Center
        • Publish Date:
        • Publish Location: ➤  Hampton, Virginia - Springfield, VA - Hampton, Va - [Springfield, Va

        “Assessment of dual-point drag reduction for an executive-jet modified airfoil section” 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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          5Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip

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          “Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip” Metadata:

          • Title: ➤  Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip
          • Author:
          • Language: English
          • Number of Pages: Median: 286
          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center - For sale by the National Technical Information Service]
          • Publish Date:
          • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

          “Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip” 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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            6Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)

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            “Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)” Metadata:

            • Title: ➤  Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)
            • Author:
            • Language: English
            • Number of Pages: Median: 44
            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
            • Publish Date:
            • Publish Location: ➤  Linthicum Heights, MD - [Springfield, Va - Hampton, Va

            “Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate)” 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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              7The boundary layer on compressor cascade blades

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              “The boundary layer on compressor cascade blades” Metadata:

              • Title: ➤  The boundary layer on compressor cascade blades
              • Author:
              • Language: English
              • Publisher: ➤  Applied Research Laboratory, The Pennsylvania State University - National Aeronautics and Space Administration
              • Publish Date:
              • Publish Location: ➤  [Washington, D.C - State College, PA

              “The boundary layer on compressor cascade blades” 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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                8Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails

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                “Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails” Metadata:

                • Title: ➤  Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
                • Publish Date:
                • Publish Location: [Springfield, Va - Hampton, Va

                “Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1997
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Access

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                  9Navier-Stokes simulation of several high-lift reference H configurations

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                  “Navier-Stokes simulation of several high-lift reference H configurations” Metadata:

                  • Title: ➤  Navier-Stokes simulation of several high-lift reference H configurations
                  • Author:
                  • Language: English
                  • Publisher: ➤  Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
                  • Publish Date:
                  • Publish Location: ➤  Hanover, MD - Hampton, Va - Springfield, VA

                  “Navier-Stokes simulation of several high-lift reference H configurations” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

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

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                    10On the modeling of low-Reynolds-number turbulence

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                    “On the modeling of low-Reynolds-number turbulence” Metadata:

                    • Title: ➤  On the modeling of low-Reynolds-number turbulence
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 135
                    • Publisher: ➤  Lewis Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                    • Publish Date:
                    • Publish Location: ➤  [Washington, DC] - Cleveland, Ohio - [Springfield, Va

                    “On the modeling of low-Reynolds-number turbulence” 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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                      11Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine

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                      “Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine” Metadata:

                      • Title: ➤  Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                      • Publish Date:
                      • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                      “Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

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

                      Online Access

                      Downloads Are Not Available:

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                        12The three-dimensional flow past a rapidly rotating circular cylinder

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                        “The three-dimensional flow past a rapidly rotating circular cylinder” Metadata:

                        • Title: ➤  The three-dimensional flow past a rapidly rotating circular cylinder
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 15
                        • Publisher: ➤  National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering - National Aeronautics and Space Administration, Langley Research Center
                        • Publish Date:
                        • Publish Location: Hampton, Va - [Springfield, Va

                        “The three-dimensional flow past a rapidly rotating circular cylinder” 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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                          13Flow-separation patterns on symmetric forebodies

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                          “Flow-separation patterns on symmetric forebodies” Metadata:

                          • Title: ➤  Flow-separation patterns on symmetric forebodies
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 135
                          • Publisher: ➤  For sale by the National Technical Information Service] - Ames Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                          • Publish Date:
                          • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif - [Washington, DC]

                          “Flow-separation patterns on symmetric forebodies” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

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

                          Online Access

                          Downloads Are Not Available:

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

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                            14User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel

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                            “User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Metadata:

                            • Title: ➤  User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
                            • Author:
                            • Language: English
                            • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration - National Technical Information Service, distributor
                            • Publish Date:
                            • Publish Location: ➤  [Washington, DC - [Springfield, Va - [Washington, DC] - Springfield, Va

                            “User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

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

                            Online Access

                            Downloads Are Not Available:

                            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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                              15IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow

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                              Book's cover

                              “IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow” Metadata:

                              • Title: ➤  IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow
                              • Author: ➤  
                              • Language: English
                              • Number of Pages: Median: 324
                              • Publisher: Kluwer Academic - Springer
                              • Publish Date:
                              • Publish Location: ➤  Dordrecht - Boston, Mass - Boston - London

                              “IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 2003
                              • Is Full Text Available: No
                              • Is The Book Public: No
                              • Access Status: No_ebook

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                              16Navier-Stokes analysis of turbine blade heat transfer

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                              “Navier-Stokes analysis of turbine blade heat transfer” Metadata:

                              • Title: ➤  Navier-Stokes analysis of turbine blade heat transfer
                              • Author:
                              • Language: English
                              • Number of Pages: Median: 19
                              • Publisher: ➤  NASA - For sale by the National Technical Information Service
                              • Publish Date:
                              • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                              “Navier-Stokes analysis of turbine blade heat transfer” 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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                                17Assessment 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

                                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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                                  18Wall-layer eruptions in turbulent flows

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                                  “Wall-layer eruptions in turbulent flows” Metadata:

                                  • Title: ➤  Wall-layer eruptions in turbulent flows
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
                                  • Publish Date:
                                  • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                  “Wall-layer eruptions in turbulent flows” 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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                                    19An application of a two-equation model of turbulence to three-dimensional chemically reacting flows

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                                    “An application of a two-equation model of turbulence to three-dimensional chemically reacting flows” Metadata:

                                    • Title: ➤  An application of a two-equation model of turbulence to three-dimensional chemically reacting flows
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                    • Publish Date:
                                    • Publish Location: ➤  Springfield, Va - [Washington, DC

                                    “An application of a two-equation model of turbulence to three-dimensional chemically reacting 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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                                      20Control of unsteady separated flow associated with the dynamic stall of airfoils

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                                      “Control of unsteady separated flow associated with the dynamic stall of airfoils” Metadata:

                                      • Title: ➤  Control of unsteady separated flow associated with the dynamic stall of airfoils
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - MCAT Institute
                                      • Publish Date:
                                      • Publish Location: ➤  Springfield, Va - [Washington, DC - Springfield, Va.? - San Jose, CA

                                      “Control of unsteady separated flow associated with the dynamic stall of airfoils” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

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

                                      Online Access

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                                        21Water-tunnel study of transition flow around circular cylinders

                                        By

                                        “Water-tunnel study of transition flow around circular cylinders” Metadata:

                                        • Title: ➤  Water-tunnel study of transition flow around circular cylinders
                                        • Author:
                                        • Language: English
                                        • Number of Pages: Median: 31
                                        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                                        • Publish Date:
                                        • Publish Location: ➤  [Springfield, Va - Washington, D.C

                                        “Water-tunnel study of transition flow around circular cylinders” 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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                                        22Reynolds-stress and dissipation rate budgets in a turbulent channel flow

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                                        “Reynolds-stress and dissipation rate budgets in a turbulent channel flow” Metadata:

                                        • Title: ➤  Reynolds-stress and dissipation rate budgets in a turbulent channel flow
                                        • Author:
                                        • Language: English
                                        • Number of Pages: Median: 38
                                        • 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

                                        “Reynolds-stress and dissipation rate budgets in a turbulent channel flow” 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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                                          23High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number

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                                          “High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number” Metadata:

                                          • Title: ➤  High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
                                          • Publish Date:
                                          • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                          “High-resolution liquid crystal heat transfer measurements on the end wall of a turbine passage with variations in Reynolds number” 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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                                            24Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels

                                            By

                                            “Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels” Metadata:

                                            • Title: ➤  Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - National Technical Information Service, distributor]
                                            • Publish Date:
                                            • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                            “Low-speed tests of a high-aspect-ratio, supercritical-wing transport model equipped with a high-lift flap system in the Langley 4- by 7-meter and Ames 12-foot pressure tunnels” 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

                                            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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                                              25A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel

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                                              • Title: ➤  A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office
                                              • Publish Date:
                                              • Publish Location: [Washington, DC]

                                              “A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel” Subjects and Themes:

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                                              26Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊

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                                              “Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊” Metadata:

                                              • Title: ➤  Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊
                                              • Author:
                                              • Language: English
                                              • Number of Pages: Median: 464
                                              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
                                              • Publish Date:
                                              • Publish Location: Washington - Springfield, Va

                                              “Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊” Subjects and Themes:

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                                              27Transonic 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:

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                                              • First Year Published: 1994
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                                                28Final report for the grant integration of viscous effects into inviscid computational methods

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                                                • Title: ➤  Final report for the grant integration of viscous effects into inviscid computational methods
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                                                • Language: English
                                                • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                • Publish Date:
                                                • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                “Final report for the grant integration of viscous effects into inviscid computational methods” Subjects and Themes:

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                                                  29Instability and transition of flow at, and near, an attachment-line

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

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

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                                                    30Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows

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                                                    • Title: ➤  Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows
                                                    • Author:
                                                    • Language: English
                                                    • Publisher: ➤  For sale by National Technical Information Service - NASA-Marshall Space Flight Center
                                                    • Publish Date:
                                                    • Publish Location: ➤  [Springfield, Va - Marshall Space Flight Center, Ala

                                                    “Velocity-pressure integrated versus penalty finite element methods for high Reynolds number flows” Subjects and Themes:

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                                                    • First Year Published: 1988
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                                                      31The effects of viscosity on the stability of a trailing-line vortex in compressible flow

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                                                      • Title: ➤  The effects of viscosity on the stability of a trailing-line vortex in compressible flow
                                                      • Author:
                                                      • Language: English
                                                      • Publisher: ➤  Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
                                                      • Publish Date:
                                                      • Publish Location: [Springfield, Va - Hampton, VA

                                                      “The effects of viscosity on the stability of a trailing-line vortex in compressible flow” Subjects and Themes:

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                                                        32Numerical simulation of internal heat transfer phenomena occurring during de-icing of aircraft components

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                                                        “Numerical simulation of internal heat transfer phenomena occurring during de-icing of aircraft components” Metadata:

                                                        • Title: ➤  Numerical simulation of internal heat transfer phenomena occurring during de-icing of aircraft components
                                                        • Author:
                                                        • Language: English
                                                        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                        • Publish Date:
                                                        • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                        “Numerical simulation of internal heat transfer phenomena occurring during de-icing of aircraft components” Subjects and Themes:

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                                                          33Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations

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                                                          “Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations” Metadata:

                                                          • Title: ➤  Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                          • Publish Date:
                                                          • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                                          “Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations” Subjects and Themes:

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                                                            34Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds

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                                                            “Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds” Metadata:

                                                            • Title: ➤  Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
                                                            • Author:
                                                            • Language: English
                                                            • Number of Pages: Median: 120
                                                            • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - Ames Research Center - For sale by the National Technical Information Service]
                                                            • Publish Date:
                                                            • Publish Location: ➤  Edwards, Calif - [Springfield, Va - [Washington, DC]

                                                            “Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds” Subjects and Themes:

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                                                            • First Year Published: 1987
                                                            • Is Full Text Available: No
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                                                              35Wing pressure distributions from subsonic tests of a high-wing transport model

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                                                              “Wing pressure distributions from subsonic tests of a high-wing transport model” Metadata:

                                                              • Title: ➤  Wing pressure distributions from subsonic tests of a high-wing transport model
                                                              • 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

                                                              “Wing pressure distributions from subsonic tests of a high-wing transport model” Subjects and Themes:

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                                                                36Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results

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                                                                “Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Metadata:

                                                                • Title: ➤  Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
                                                                • 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

                                                                “Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Subjects and Themes:

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                                                                • First Year Published: 1997
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                                                                  37Flight Mechanics/Estimation Theory Symposium, 1989

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                                                                  • Title: ➤  Flight Mechanics/Estimation Theory Symposium, 1989
                                                                  • Author: ➤  
                                                                  • Language: English
                                                                  • Number of Pages: Median: 476
                                                                  • Publisher: ➤  For sale by the National Technical Information Service, distributor - NASA, Office of Management, Scientific and Technical Information Division - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
                                                                  • Publish Date:
                                                                  • Publish Location: ➤  [Washington, DC] - Washington, D.C.] - [Springfield, Va

                                                                  “Flight Mechanics/Estimation Theory Symposium, 1989” Subjects and Themes:

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                                                                    38Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

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                                                                    “Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel” Metadata:

                                                                    • Title: ➤  Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
                                                                    • Author:
                                                                    • Language: English
                                                                    • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                                                                    • Publish Date:
                                                                    • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                                                    “Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel” Subjects and Themes:

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                                                                    • First Year Published: 1985
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                                                                      39Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing

                                                                      By

                                                                      “Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing” Metadata:

                                                                      • Title: ➤  Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
                                                                      • Author:
                                                                      • Language: English
                                                                      • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
                                                                      • Publish Date:
                                                                      • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                                                      “Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing” Subjects and Themes:

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                                                                      • First Year Published: 1997
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                                                                        40Drag reduction on circular cylinders by ejecting jet from rear stagnation region

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                                                                        “Drag reduction on circular cylinders by ejecting jet from rear stagnation region” Metadata:

                                                                        • Title: ➤  Drag reduction on circular cylinders by ejecting jet from rear stagnation region
                                                                        • Author:
                                                                        • Language: English
                                                                        • Publisher: ➤  Dept. of Mechanical Engineering, College of Engineering and Technology, Old Dominion University - National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                        • Publish Date:
                                                                        • Publish Location: ➤  Springfield, Va - [Washington, DC - Norfolk, Va

                                                                        “Drag reduction on circular cylinders by ejecting jet from rear stagnation region” Subjects and Themes:

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                                                                        • First Year Published: 1997
                                                                        • Is Full Text Available: No
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                                                                          41Water-tunnel study of transition flow around circular cylinders

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                                                                          • Title: ➤  Water-tunnel study of transition flow around circular cylinders
                                                                          • Author:
                                                                          • Language: English
                                                                          • Number of Pages: Median: 31
                                                                          • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                                                                          • Publish Date:
                                                                          • Publish Location: ➤  [Springfield, Va - Washington, D.C

                                                                          “Water-tunnel study of transition flow around circular cylinders” Subjects and Themes:

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                                                                          • First Year Published: 1984
                                                                          • Is Full Text Available: No
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                                                                          42Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel

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                                                                          “Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel” Metadata:

                                                                          • Title: ➤  Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel
                                                                          • Author:
                                                                          • Language: English
                                                                          • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                                                                          • Publish Date:
                                                                          • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                                                          “Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel” Subjects and Themes:

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                                                                          • First Year Published: 1985
                                                                          • Is Full Text Available: No
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                                                                            43Computations of complex three-dimensional turbulent free jets

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                                                                            • Title: ➤  Computations of complex three-dimensional turbulent free jets
                                                                            • Author:
                                                                            • Language: English
                                                                            • Publisher: ➤  Institute for Computational and Applied Mechanics, Old Dominion University - National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                            • Publish Date:
                                                                            • Publish Location: ➤  Norfolk, Va - [Washington, DC - Springfield, Va

                                                                            “Computations of complex three-dimensional turbulent free jets” Subjects and Themes:

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                                                                            • First Year Published: 1997
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                                                                              44Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers

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                                                                              “Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers” Metadata:

                                                                              • Title: ➤  Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers
                                                                              • Author:
                                                                              • Language: English
                                                                              • Number of Pages: Median: 19
                                                                              • Publisher: ➤  U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories
                                                                              • Publish Date:
                                                                              • Publish Location: Boulder, Colo

                                                                              “Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers” Subjects and Themes:

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                                                                              • First Year Published: 1980
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                                                                              45Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions

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

                                                                              • Title: ➤  Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions
                                                                              • Author:
                                                                              • Language: English
                                                                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                                                                              • Publish Date:
                                                                              • Publish Location: Hampton, Va - [Springfield, Va

                                                                              “Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions” Subjects and Themes:

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                                                                              • First Year Published: 1999
                                                                              • Is Full Text Available: No
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                                                                                46Viscous flow in a rectangular cut-out

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                                                                                “Viscous flow in a rectangular cut-out” Metadata:

                                                                                • Title: ➤  Viscous flow in a rectangular cut-out
                                                                                • Author:
                                                                                • Language: English
                                                                                • Number of Pages: Median: 39
                                                                                • Publisher: ➤  Dept. of Mechanical Engineering, Faculty of Applied Science, University of British Columbia
                                                                                • Publish Date:
                                                                                • Publish Location: [Vancouver]

                                                                                “Viscous flow in a rectangular cut-out” Subjects and Themes:

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                                                                                • First Year Published: 1965
                                                                                • Is Full Text Available: No
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                                                                                47Evaluation of high reynolds number flow in a 180 degree turn-around duct

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                                                                                “Evaluation of high reynolds number flow in a 180 degree turn-around duct” Metadata:

                                                                                • Title: ➤  Evaluation of high reynolds number flow in a 180 degree turn-around duct
                                                                                • Author:
                                                                                • Language: English
                                                                                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                                                • Publish Date:
                                                                                • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                                                “Evaluation of high reynolds number flow in a 180 degree turn-around duct” Subjects and Themes:

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                                                                                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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                                                                                  48Flow distribution around the SSME main injector assembly using porosity formulation

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                                                                                  “Flow distribution around the SSME main injector assembly using porosity formulation” Metadata:

                                                                                  • Title: ➤  Flow distribution around the SSME main injector assembly using porosity formulation
                                                                                  • Author:
                                                                                  • Language: English
                                                                                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                                  • Publish Date:
                                                                                  • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                                                  “Flow distribution around the SSME main injector assembly using porosity formulation” 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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                                                                                  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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                                                                                    49Experimental measurements of sonic boom signatures using a continuous data acquistion technique

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                                                                                    “Experimental measurements of sonic boom signatures using a continuous data acquistion technique” Metadata:

                                                                                    • Title: ➤  Experimental measurements of sonic boom signatures using a continuous data acquistion technique
                                                                                    • Author:
                                                                                    • Language: English
                                                                                    • Number of Pages: Median: 45
                                                                                    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                                                                                    • Publish Date:
                                                                                    • Publish Location: Hampton, Virginia

                                                                                    “Experimental measurements of sonic boom signatures using a continuous data acquistion technique” Subjects and Themes:

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                                                                                    Access and General Info:

                                                                                    • First Year Published: 2013
                                                                                    • Is Full Text Available: No
                                                                                    • Is The Book Public: No
                                                                                    • Access Status: No_ebook

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                                                                                    50Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers

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                                                                                    “Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers” Metadata:

                                                                                    • Title: ➤  Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers
                                                                                    • Author:
                                                                                    • Language: English
                                                                                    • Number of Pages: Median: 19
                                                                                    • Publisher: ➤  U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories
                                                                                    • Publish Date:
                                                                                    • Publish Location: Boulder, Colo

                                                                                    “Effects of large-scale intermittency of turbulence on scalar spectra at high wave numbers” Subjects and Themes:

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                                                                                    Access and General Info:

                                                                                    • First Year Published: 1980
                                                                                    • Is Full Text Available: Yes
                                                                                    • Is The Book Public: Yes
                                                                                    • Access Status: Public

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