Effect of leading-edge load constraints on the design and performance of supersonic wings / Christine M. Carden.
|Main Author:||Darden, Christine M.|
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1985.
> Design and construction.
Leading edges (Aerodynamics)
Airplanes > Wings > Testing > Statistics.
Prepared at Langley Research Center.
iii, 74 p. :
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