Investigation of lift and center of pressure of low-aspect-ratio, cruciform, triangular, and rectangular wings in combination with a slender fuselage at high supersonic speeds

Thomas N. Canning, Billy Pat Denardo
naca-rm-a52c24
Jun 1952


Tests were conducted in the Ames supersonic free-flight wind tunnel to evaluate the usefulness of available theory for the calculation of lift-curve slope and center of pressure of low-aspect-ratio, triangular, and rectangular cruciform wings in combination with a long slender body.

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