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Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method

Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method - - Washington, D.C. National Aeronautics and Space Administration 1986 - 185 p. - NASA TP 2628 : 1986 .

ISBN:

Subjects--Topical Terms:

Forward-swept wings, Transonic wing design, Maneuvering aerodynamics, Maneuvering aircraft, Transonic wings

Universal Decimal Class. No.: LNASA TP 2628 : 1986

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