General solutions for flow past slender cambered wings with swept trailing edges and calculation of additional loading due to control surfaces

E. B. Klunker, Keith C. Harder
naca-tn-4242
May 1958


The slender-wing-type analysis is used to obtain general expressions for the surface pressure, lift, and rolling moment for cambered wings with swept trailing edges. These results are specialized to give the additional loading due to the deflection of trailing-edge control surfaces and the loading due to a particular type of wing twist.

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