Computational Study of a Conical Wing Having Unit Aspect Ratio at Supersonic Speeds
11th Conference, Applied aerodynamics ; 1993 ; Monterey; CA
01.01.1993
13 pages
In 2 vols. Paper nos 93-3400 to 93-3538 with gaps bound in 2 vols
Aufsatz (Konferenz)
Englisch
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Computational Study of a Conical Unit Aspect Ratio Wing at Supersonic Speeds
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