NSWCDM computer program calculates aerodynamic loading and pressure distributions on supersonic configurations consisting of axisymmetric bodies with cruciform or planar canard and tail fins. Versatile program allows for configuration pitched and rolled, and fins deflected. Tail fins are interdigitated with respect to forward fins.
Loads and Pressures on Axisymmetric Bodies with Cruciform Fins
NASA Tech Briefs ; 7 , 2
01.05.1983
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Englisch
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