Item Details

Flight Test and Analysis of the Rolling Motions of a 79 ̊Clipped Delta Configuration With Wing-Tip Fins at Supersonic Speeds

James L. Raper
Format
Book; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, 1963.
Language
English
Variant Title
NASA TN D-2017
Series
NASA Technical Note
Description
54 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
Includes bibliographical references (p. 20).
Series Statement
NASA technical note ; D-2017
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Flight test and analysis of the rolling motions of a 79 ̊clipped delta configuration with wing-tip fins at supersonic speeds / c| James L. Raper.
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    a| NASA TN D-2017
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    a| Washington, D.C. : b| National Aeronautics and Space Administration, c| 1963.
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    a| 54 p. : b| ill. ; c| 27 cm.
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    a| NASA technical note ; v| D-2017
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    a| Includes bibliographical references (p. 20).
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    a| Mode of access: Internet.
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    a| Aerodynamics, Supersonic.
    650
      
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    a| Equations of speed.
    650
      
    0
    a| Delta wing airplanes.
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    0
    a| Airplanes x| Flight testing.
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    a| Langley Research Center.
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