Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile

Robert W. Rainey
naca-rm-l50i29a
Mar 1951


having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 The lift, drag, and pitching-moment measurements from tests made in the Langley 9-inch supersonic tunnel of four missile configurations having wing-tail-span ratios less than 1 are presented. These configurations incorporated changes to wing and tail plan form and wing-tail-span ratios.

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