Item Details

Low-Speed Effects of High-Lift Devices on the Aerodynamic Characteristics of a Supersonic Transport Model With Outboard Tails

by William C. Sleeman, Jr., Edward J. Ray and Paul G. Fournier
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, 1963.
Language
English
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:X-895
Description
24 p. : ill. ; 26 cm.
Mode of access: Internet.
Notes
  • "October 1963."
  • Cover title.
  • Includes bibliographical references (p. 6).
Series Statement
NASA technical memorandum ; X-895
Other Forms
Full text also available online. Address as of 11/18/2010: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19670022813_1967022813.pdf.
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Low-speed effects of high-lift devices on the aerodynamic characteristics of a supersonic transport model with outboard tails / c| by William C. Sleeman, Jr., Edward J. Ray and Paul G. Fournier.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration, c| 1963.
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    a| 24 p. : b| ill. ; c| 26 cm.
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    a| "October 1963."
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    a| Includes bibliographical references (p. 6).
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    a| Full text also available online. Address as of 11/18/2010: u| http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19670022813_1967022813.pdf.
    538
      
      
    a| Mode of access: Internet.
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    a| Supersonic wind tunnels x| Testing.
    650
      
    0
    a| Trailing edge flaps.
    650
      
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    a| Stability of airplanes, Lateral.
    650
      
    0
    a| Stability of airplanes, Longitudinal.
    650
      
    0
    a| Airplanes x| Wings, Swept-back x| Stability x| Testing.
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    a| Fournier, Paul G.
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    a| Ray, Edward J.
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    a| Langley Research Center.
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    b| UIU c| UIUC d| 20170509 s| google u| uiug.30112104504854 y| 1963 r| pd q| bib

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