Explore: Camber (aerofoils)

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Source: The Open Library

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1Effects of longitudinal elastic camber on slender aircraft in steady symmetrical flight

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“Effects of longitudinal elastic camber on slender aircraft in steady symmetrical flight” Metadata:

  • Title: ➤  Effects of longitudinal elastic camber on slender aircraft in steady symmetrical flight
  • Author:
  • Language: English
  • Number of Pages: Median: 95
  • Publisher: H.M.S.O.
  • Publish Date:
  • Publish Location: London
  • Dewey Decimal Classification:
  • Library of Congress Classification: TL-0526.00000000.G7 A4 no. 3426

“Effects of longitudinal elastic camber on slender aircraft in steady symmetrical flight” Subjects and Themes:

Edition Identifiers:

  • The Open Library ID: OL5566196M
  • Online Computer Library Center (OCLC) ID: 6188134
  • Library of Congress Control Number (LCCN): 67071453

Book Classifications

Access and General Info:

  • First Year Published: 1966
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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2Numerical analysis of a variable camber rotor blade as a lift cotrol device

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“Numerical analysis of a variable camber rotor blade as a lift cotrol device” Metadata:

  • Title: ➤  Numerical analysis of a variable camber rotor blade as a lift cotrol device
  • Author:
  • Language: English
  • Publisher: ➤  Flight Research Laboratory, University of Kansas Center for Research, Inc. - National Aeronautics and Space Administration, Ames Research Center
  • Publish Date:
  • Publish Location: ➤  [Moffett Field, Calif - Lawrence, Kans

“Numerical analysis of a variable camber rotor blade as a lift cotrol device” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1984
  • 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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    3Calculation of vortex lift effect for cambered wings by the suction analogy

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    “Calculation of vortex lift effect for cambered wings by the suction analogy” Metadata:

    • Title: ➤  Calculation of vortex lift effect for cambered wings by the suction analogy
    • Author:
    • Language: English
    • Number of Pages: Median: 83
    • 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

    “Calculation of vortex lift effect for cambered wings by the suction analogy” 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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    4Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration

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    “Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration” Metadata:

    • Title: ➤  Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration
    • Author:
    • Language: English
    • Number of Pages: Median: 91
    • 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

    “Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration” 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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    5Production version of the extended NASA-Langley Vortex Lattice FORTRAN Computer Program

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    “Production version of the extended NASA-Langley Vortex Lattice FORTRAN Computer Program” Metadata:

    • Title: ➤  Production version of the extended NASA-Langley Vortex Lattice FORTRAN Computer Program
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va

    “Production version of the extended NASA-Langley Vortex Lattice FORTRAN Computer Program” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1982
    • 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

      Find Production version of the extended NASA-Langley Vortex Lattice FORTRAN Computer Program at online marketplaces:


      6Delta wings with longitudinal camber at low speed

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      “Delta wings with longitudinal camber at low speed” Metadata:

      • Title: ➤  Delta wings with longitudinal camber at low speed
      • Author:
      • Language: English
      • Number of Pages: Median: 18
      • Publisher: H.M. Stationery Off.
      • Publish Date:
      • Publish Location: London
      • Dewey Decimal Classification: 629.13008 s
      • Library of Congress Classification: TL-0507.00000000.G77 no. 1129

      “Delta wings with longitudinal camber at low speed” Subjects and Themes:

      Edition Identifiers:

      Book Classifications

      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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      7Camber effects on the non-linear lift of slender wings with sharp leading edges

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      “Camber effects on the non-linear lift of slender wings with sharp leading edges” Metadata:

      • Title: ➤  Camber effects on the non-linear lift of slender wings with sharp leading edges
      • Author:
      • Language: English
      • Number of Pages: Median: 18
      • Publisher: H.M.S.O.
      • Publish Date:
      • Publish Location: London
      • Dewey Decimal Classification: 629.13432
      • Library of Congress Classification: TL-0507.00000000.G77 no. 924

      “Camber effects on the non-linear lift of slender wings with sharp leading edges” Subjects and Themes:

      Edition Identifiers:

      Book Classifications

      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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