Tests of Aerodynamically Heated Multiweb Wing Structures in a Free Jet at Mach Number 2: Five Aluminum-alloy Models of 20-inch Chord with 0.064-inch-thick Skin, 0.025-inch-thick Webs, and Various Chordwise Stiffening at 2 Angle of Attack

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National Aeronautics and Space Administration, 1960 - Aerodynamic heating - 33 pages
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