AIAA-2006-6636 Sonic Boom Mitigation Through Thickness, Camber and Nose Angle Optimizations for a Delta Wing
AIAA atmospheric flight mechanics conference ; 2006 ; Keystone, Colo
01.01.2006
12 pages
Paper numbers 2006-6000 to 2006-6834 with gaps held
Aufsatz (Konferenz)
Englisch
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