Item Details

Effect of Wing Location and Strakes on Stability and Control Characteristics of a Monoplanar Circular Missile With Low-Profile Tail Fins at Supersonic Speeds

A.B. Blair, Jr.
Format
Book; Government Document
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980.
Language
English
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:81878
Description
197 p. : chiefly ill. ; 27 cm.
Notes
  • "Langley Research Center."
  • Dec. 1980.
  • Includes bibliographical references.
Series Statement
NASA technical memorandum 81878
Technical Details
  • Access in Virgo Classic

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    a| Guided missiles x| Wings.
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    a| Supersonic wind tunnels.
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    a| Rolling (Aerodynamics)
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    a| Yawing (Aerodynamics)
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    a| Stability of airplanes, Lateral.
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