Comparison between theory and experiment for interference pressure field between wing and body at supersonic speeds

William C. Pitts, Jack N. Nielsen, Maurice P. Gionfriddo
naca-tn-3128
Apr 1954


Pressure-distribution data were obtained for a wing-body combination at Mach numbers of 1.48 and 2.00 and at Reynolds numbers of 0.6, 1.2, and 1.5 X 10(exp 6) to investigate the effects of wing-body interference.

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