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.
|Main Author:||Blair, A. B.|
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1980.
Stability of airplanes, Lateral.
Supersonic wind tunnels.
Guided missiles > Guided missiles / Wings.
"Langley Research Center."
197 p. :
chiefly ill. ;
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