Division of load among the wing, fuselage, and tail of aircraft

John P. Mayer, Clarence L. Gillis
naca-rm-l51e14a
May 1951


Data are presented for the division of load among the wing, fuselage and tail for several aircraft configurations at subsonic and supersonic speeds. These data were obtained on full-scale airplanes, rocket-propelled models, and in low-speed wind-tunnel tests.

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