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Wing planform effects at supersonic speeds for an advanced fighter configuration

Wing planform effects at supersonic speeds for an advanced fighter configuration - - Washington, D.C. National Aeronautics & Space Administration 1984 - 115 p. - NASA TP 2269 : 1983 .

ISBN:

Subjects--Topical Terms:

Supersonic aerodyn, Planform study, Cranked wings, Internal flow

Universal Decimal Class. No.: LNASA TP 2269 : 1983

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