Tests of aerodynamically heated multiweb wing structures in a free jet at Mach number 2 : two aluminum-alloy models of 20-inch chord with 0.064-inch-thick skin at angles of attack of 0 degree and plus or minus 2 degrees

Miltonberger, Georgene H Davidson, John R Griffith, George E
naca-rm-l57h19
October 28, 1957


No Abstract Available

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