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Source: The Open Library

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1Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration

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“Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration” Metadata:

  • Title: ➤  Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration
  • Author:
  • Language: English
  • Number of Pages: Median: 30
  • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center
  • Publish Date:
  • Publish Location: ➤  Hampton, Va - [Springfield, Va - Washington, D.C

“Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration” 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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    2Performance validation of the ANSER control laws for the F-18 HARV

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    “Performance validation of the ANSER control laws for the F-18 HARV” Metadata:

    • Title: ➤  Performance validation of the ANSER control laws for the F-18 HARV
    • 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

    “Performance validation of the ANSER control laws for the F-18 HARV” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

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

    Online Access

    Downloads Are Not Available:

    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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      3Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data

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      “Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data” Metadata:

      • Title: ➤  Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from 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

      “Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

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

      Online Access

      Downloads Are Not Available:

      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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        4Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV

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        “Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV” Metadata:

        • Title: ➤  Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

        “Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV” 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:

        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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          5Water tunnel flow visualization study of a 4.4% scale X-31 forebody

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          “Water tunnel flow visualization study of a 4.4% scale X-31 forebody” Metadata:

          • Title: ➤  Water tunnel flow visualization study of a 4.4% scale X-31 forebody
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
          • Publish Date:
          • Publish Location: ➤  Edwards, Calif - [Springfield, Va

          “Water tunnel flow visualization study of a 4.4% scale X-31 forebody” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

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

          Online Access

          Downloads Are Not Available:

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

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            6Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters

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            “Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters” Metadata:

            • Title: ➤  Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters
            • Author:
            • Language: English
            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
            • Publish Date:
            • Publish Location: ➤  [Washington, DC] - [Springfield, Va

            “Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters” 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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              7Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing

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              “Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing” Metadata:

              • Title: ➤  Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing
              • Author:
              • Number of Pages: Median: 167
              • Publisher: Langley Research Center
              • Publish Date:
              • Publish Location: Hampton, Va

              “Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

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

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              8Exploratory investigation of forebody strakes for yaw control of a generic fighter with a symmetric 60⁰ half-angle chine forebody

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              “Exploratory investigation of forebody strakes for yaw control of a generic fighter with a symmetric 60⁰ half-angle chine forebody” Metadata:

              • Title: ➤  Exploratory investigation of forebody strakes for yaw control of a generic fighter with a symmetric 60⁰ half-angle chine forebody
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: [Springfield, Va - Hampton, Va

              “Exploratory investigation of forebody strakes for yaw control of a generic fighter with a symmetric 60⁰ half-angle chine forebody” 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

              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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