Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper : Mach lines behind flap leading and trailing edges

Julian H. Kainer, Jack E. Marte
Oct 1950

Generalized expressions in closed form have been obtained by means of linearized theory for the aerodynamic characteristics (lift-, rolling-moment, pitching-moment-, and hinge-moment-coefficient derivatives) due to deflection of inboard trailing-edge flaps.

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