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
naca-tn-2205
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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