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- W2289845807 abstract "AT TRANSONIC SPEEDS By Claude V. Williams and Richard E. KuhnSUMMARY A study of the aerodynamic loads on sweptback wings at transonic speeds has indicated that, for thick wings, the spanwise center of pres-sure moves inward, whereas for thin wings, the center of pressure moves outward with increase in Mach number; and increases in the sweep angle of a thin wing cause the spanwise center of pressure to move progres-sively outboard. Washing out a thin swept wing to approximate the effects of aeroelastic twisting shifted the spanwise center of pressure inboard and at a Mach number of 1.00, this shift was primarily due to the loss in load over the trailing edges of the outboard portions of the span. An investigation of the effects of sideslip on the loads over a swept-wing—curved-body combination indicated that increase in sideslip angle increased the relative load over the forward wing such that even though the spanwise center of pressure of the wing remained constant, the root bending-moment coefficients were increased." @default.
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- W2289845807 date "1958-01-01" @default.
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- W2289845807 title "NACA RESEARCH MEMORANDUM" @default.
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