Tests of Aerodynamically Heated Multiweb Wing Structures in a Free Jet at Mach Number 2 : Four Aluminum-alloy Models of 20-inch Chord and Span with 0.064-inch-thick Skin, 0.025-inch-thick Ribs and Webs, and Zero, One, Two, or Three Chordwise Ribs
08.05.1958
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Englisch