Explore: Jet Flaps (airplanes)

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Source: The Open Library

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Search results from The Open Library

1Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee

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“Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee” Metadata:

  • Title: ➤  Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee
  • Author:
  • Language: English
  • Number of Pages: Median: 77
  • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: Washington - Springfield, Va

“Low-speed wind-tunnel investigation of a swept-wing model having distributed upper-surface blowing near the wing leading edge or at the flap knee” 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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2A flight investigation of the stability, control, and handling qualities of an augumented jet flap STOL airplane

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“A flight investigation of the stability, control, and handling qualities of an augumented jet flap STOL airplane” Metadata:

  • Title: ➤  A flight investigation of the stability, control, and handling qualities of an augumented jet flap STOL airplane
  • Author:
  • Language: English
  • Number of Pages: Median: 140
  • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
  • Publish Date:
  • Publish Location: [Washington] - Springfield, Va

“A flight investigation of the stability, control, and handling qualities of an augumented jet flap STOL airplane” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1978
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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3Experimental study of acoustic loads on upper-surface-blown STOL airplane configuration

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“Experimental study of acoustic loads on upper-surface-blown STOL airplane configuration” Metadata:

  • Title: ➤  Experimental study of acoustic loads on upper-surface-blown STOL airplane configuration
  • Author:
  • Language: English
  • Number of Pages: Median: 54
  • 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 study of acoustic loads on upper-surface-blown STOL airplane configuration” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1979
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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4The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane

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“The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane” Metadata:

  • Title: ➤  The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane
  • Author:
  • Language: English
  • Number of Pages: Median: 56
  • 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

“The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane” 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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5A flight investigation of the stability, control, and handling qualities of an augumented jet flap STOL airplane

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“A flight investigation of the stability, control, and handling qualities of an augumented jet flap STOL airplane” Metadata:

  • Title: ➤  A flight investigation of the stability, control, and handling qualities of an augumented jet flap STOL airplane
  • Author:
  • Language: English
  • Number of Pages: Median: 140
  • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
  • Publish Date:
  • Publish Location: Springfield, Va - [Washington]

“A flight investigation of the stability, control, and handling qualities of an augumented jet flap STOL airplane” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1978
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

Online Marketplaces

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6Velocity and temperature decay characteristics of inverted-profile jets

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“Velocity and temperature decay characteristics of inverted-profile jets” Metadata:

  • Title: ➤  Velocity and temperature decay characteristics of inverted-profile jets
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
  • Publish Date:
  • Publish Location: [Cleveland, Ohio

“Velocity and temperature decay characteristics of inverted-profile jets” 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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    7Subsonic maneuver capability of a supersonic cruise fighter wing concept

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    “Subsonic maneuver capability of a supersonic cruise fighter wing concept” Metadata:

    • Title: ➤  Subsonic maneuver capability of a supersonic cruise fighter wing concept
    • Author:
    • Language: English
    • 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, DC]

    “Subsonic maneuver capability of a supersonic cruise fighter wing concept” 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:

      Online Marketplaces

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      8Finite element analysis of aeronacoustic jet-flap flows

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      “Finite element analysis of aeronacoustic jet-flap flows” Metadata:

      • Title: ➤  Finite element analysis of aeronacoustic jet-flap flows
      • Author:
      • Language: English
      • Number of Pages: Median: 64
      • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
      • Publish Date:
      • Publish Location: [Washington] - Springfield, Va

      “Finite element analysis of aeronacoustic jet-flap 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

      Online Marketplaces

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      9Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model

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      “Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model” Metadata:

      • Title: ➤  Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model
      • Author:
      • Language: English
      • Number of Pages: Median: 22
      • Publisher: H.M.S.O.
      • Publish Date:
      • Publish Location: London

      “Low-speed wind-tunnel measurements of damping in yaw (n[psi]) on an A.R. 9 jet-flap complete model” Subjects and Themes:

      Edition Identifiers:

      • The Open Library ID: OL5586072M
      • Online Computer Library Center (OCLC) ID: 6163138
      • Library of Congress Control Number (LCCN): 67104629

      Access and General Info:

      • First Year Published: 1967
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Marketplaces

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      10The oscillating jet flap

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      Book's cover

      “The oscillating jet flap” Metadata:

      • Title: The oscillating jet flap
      • Author:
      • Language: English
      • Number of Pages: Median: 39
      • Publisher: Naval Postgraduate School
      • Publish Date:
      • Publish Location: Monterey, Calif

      “The oscillating jet flap” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1976
      • Is Full Text Available: Yes
      • Is The Book Public: Yes
      • Access Status: Public

      Online Access

      Downloads:

        Online Borrowing:

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