Explore: Tail Surfaces

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Source: The Open Library

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Search results from The Open Library

1Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics

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“Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics” Metadata:

  • Title: ➤  Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
  • Author:
  • Language: English
  • Number of Pages: Median: 103
  • 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

“Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics” Subjects and Themes:

Edition Identifiers:

Access and General Info:

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

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2Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements

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“Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements” Metadata:

  • Title: ➤  Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements
  • Author:
  • Language: English
  • Number of Pages: Median: 44
  • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
  • Publish Date:
  • Publish Location: ➤  Washington, D.C - [Springfield, Va

“Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1981
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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3NASA/FAA Tailplane Icing Program overview

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“NASA/FAA Tailplane Icing Program overview” Metadata:

  • Title: ➤  NASA/FAA Tailplane Icing Program overview
  • Author:
  • Language: English
  • Number of Pages: Median: 153
  • Publisher: ➤  Available from NASA Center for Aerospace Information - National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center - National Aeronautics and Space Administration, Glenn Research Center
  • Publish Date:
  • Publish Location: ➤  Hanover, Md - [Springfield, Va - [Cleveland, Ohio]

“NASA/FAA Tailplane Icing Program overview” 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.

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    4A low-speed wind-tunnel investigation of the tailplane effectiveness of a model representing the airbus type of aircraft

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    “A low-speed wind-tunnel investigation of the tailplane effectiveness of a model representing the airbus type of aircraft” Metadata:

    • Title: ➤  A low-speed wind-tunnel investigation of the tailplane effectiveness of a model representing the airbus type of aircraft
    • Author:
    • Language: English
    • Number of Pages: Median: 40
    • Publisher: H.M. Stationery Off.
    • Publish Date:
    • Publish Location: London

    “A low-speed wind-tunnel investigation of the tailplane effectiveness of a model representing the airbus type of aircraft” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1970
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    5Prediction of light aircraft horizontal tail onset flows

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    “Prediction of light aircraft horizontal tail onset flows” Metadata:

    • Title: ➤  Prediction of light aircraft horizontal tail onset flows
    • Author:
    • Language: English
    • Number of Pages: Median: 121
    • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: Washington - Springfield, Va

    “Prediction of light aircraft horizontal tail onset flows” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1977
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    6Development of a reduced area horizontal tail for a wide body jet aircraft

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    “Development of a reduced area horizontal tail for a wide body jet aircraft” Metadata:

    • Title: ➤  Development of a reduced area horizontal tail for a wide body jet aircraft
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va

    “Development of a reduced area horizontal tail for a wide body jet aircraft” 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

    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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      7Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics

      By

      “Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics” Metadata:

      • Title: ➤  Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
      • Author:
      • Language: English
      • Number of Pages: Median: 103
      • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
      • Publish Date:
      • Publish Location: ➤  Washington, D.C - [Springfield, Va

      “Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics” 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 Marketplaces

      Find Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics at online marketplaces:


      8Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics

      By

      “Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics” Metadata:

      • Title: ➤  Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
      • Author:
      • Language: English
      • Number of Pages: Median: 103
      • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
      • Publish Date:
      • Publish Location: ➤  Washington, D.C - [Springfield, Va

      “Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics” 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 Marketplaces

      Find Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics at online marketplaces:


      9Computation and validation of fluid/structure twin tail buffet response

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      “Computation and validation of fluid/structure twin tail buffet response” Metadata:

      • Title: ➤  Computation and validation of fluid/structure twin tail buffet response
      • Author:
      • Language: English
      • Number of Pages: Median: 10
      • Publisher: ➤  National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: [Washington, D.C

      “Computation and validation of fluid/structure twin tail buffet response” 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.

      Online Borrowing:

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        10Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow

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        “Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow” Metadata:

        • Title: ➤  Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow
        • Author:
        • Language: English
        • Number of Pages: Median: 15
        • Publisher: ➤  National Aeronautics and Space Administration
        • Publish Date:
        • Publish Location: [Washington, D.C

        “Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow” 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.

        Online Borrowing:

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          11Application of linear quadratic control in reduction of aerodynamic forces on aircraft

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          “Application of linear quadratic control in reduction of aerodynamic forces on aircraft” Metadata:

          • Title: ➤  Application of linear quadratic control in reduction of aerodynamic forces on aircraft
          • Author:
          • Language: English
          • Number of Pages: Median: 267
          • Publish Date:

          “Application of linear quadratic control in reduction of aerodynamic forces on aircraft” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1980
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Marketplaces

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          12Hook code

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          “Hook code” Metadata:

          • Title: Hook code
          • Author:
          • Language: English
          • Number of Pages: Median: 259
          • Publisher: P. Martin
          • Publish Date:
          • Publish Location: ➤  Tacoma, WA (1991 Martin Slides, 812 E. 55th St., Tacoma 98404)

          “Hook code” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

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

          Online Marketplaces

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          13An investigation of the rolling moments due to side-slip on high tailplanes

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          “An investigation of the rolling moments due to side-slip on high tailplanes” Metadata:

          • Title: ➤  An investigation of the rolling moments due to side-slip on high tailplanes
          • Author:
          • Language: English
          • Number of Pages: Median: 21
          • Publisher: H.M.S.O.
          • Publish Date:
          • Publish Location: London

          “An investigation of the rolling moments due to side-slip on high tailplanes” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1968
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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