Explore: Tail Surfaces

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Books Results

Source: The Open Library

The Open Library Search Results

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.

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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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          Wiki

          Source: Wikipedia

          Wikipedia Results

          Search Results from Wikipedia

          V-tail

          unconventional arrangement of the tail control surfaces that replaces the traditional vertical and horizontal surfaces with two surfaces set in a V-shaped configuration

          Empennage

          stabilising surfaces which stabilise the flight dynamics of yaw and pitch, as well as housing control surfaces. In spite of effective control surfaces, many

          Lockheed Martin X-44 MANTA

          derived from the F-22 Raptor and featured a stretched delta wing without tail surfaces. NASA and the U.S. Air Force had begun preliminary work on the aircraft

          Flight control surfaces

          control surfaces are generally operated by dedicated aircraft flight control systems. Development of an effective set of flight control surfaces was a critical

          Tuskegee Airmen

          schemes, with red propeller spinners, yellow wing bands, and all-red tail surfaces. The Tuskegee Airmen were the first African-American military aviators

          Twin tail

          twin tail is the triple tail, but the twin-boom arrangement can also be considered a variation of the twin tail. Separating the control surfaces allows

          Convair B-36 Peacemaker variants

          FICON testing. YB-60 Modified version of the B-36 with swept wings and tail surfaces and powered by eight J-57-P-3 engines for evaluation against the B-52

          Heinkel He 177 Greif

          complained of some vibration in the airscrew shafts, the inadequacy of the tail surfaces under certain conditions, and some flutter which accompanied any vigorous

          Stabilator

           78. ISBN 978-1-107-32019-2. Retrieved 17 October 2022. All-movable tail surfaces became interesting... when high Mach number theory and transonic wind-tunnel

          Stabilizer (aeronautics)

          An aircraft stabilizer is an aerodynamic surface, typically including one or more movable control surfaces, that provides longitudinal (pitch) and/or