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Source: The Open Library

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1Optimal pitch thrust-vector angle and benefits for all flight regimes

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“Optimal pitch thrust-vector angle and benefits for all flight regimes” Metadata:

  • Title: ➤  Optimal pitch thrust-vector angle and benefits for all flight regimes
  • Author:
  • Language: English
  • Number of Pages: Median: 22
  • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Edwards, Calif

“Optimal pitch thrust-vector angle and benefits for all flight regimes” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 2000
  • 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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    2Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct

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    “Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct” Metadata:

    • Title: ➤  Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct
    • 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

    “Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct” 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

    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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      3Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)

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      “Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)” Metadata:

      • Title: ➤  Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - [Washington, DC

      “Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)” 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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        4Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance

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        “Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance” Metadata:

        • Title: ➤  Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - Edwards, Calif

        “Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance” 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

        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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          5An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities

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          “An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities” Metadata:

          • Title: ➤  An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

          “An investigation of the effects of pitch-roll (de)coupling on helicopter handling qualities” 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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            6Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations

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            “Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations” Metadata:

            • Title: ➤  Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
            • 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

            “Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

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

            Online Access

            Downloads Are Not Available:

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

            Online Borrowing:

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              Find Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations at online marketplaces:


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