Wing Design for Supersonic Aircraft with the Maximum Lift-to-Drag Ratio
8th, International conference on the methods of aerophysical research ; 1996 ; Novosibirsk, Russia
01.01.1996
5 pages
Also known as ICMAR 8
Aufsatz (Konferenz)
Englisch
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Maximum lift-to-drag ratio airfoils at moderate supersonic speeds
Engineering Index Backfile | 1969
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