AeronauticsOther - NASA Memorandum (MEMO)
FLIGHT-DETERMINED STABILITY AND CONTROL DERIVATIVES OF A SUPERSONIC AIRPLANE WITH A LOW-ASPECT-RATIO UNSWEPT WING AND A TEE-TAIL
20191 min read16 words
Andrews, W. H. and Rediess, H. A.
Legacy CDMS
Flight-determined stability & control derivatives of supersonic aircraft with low aspect ratio unswept wing & t-tail
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