NASA / TM X-186
Trussell,Donald H
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...ANGLE OF ATTACK
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.- Nasa, Washington, D.C., 1960
.- 33 .
Bound With Nasa Tm X-182-83,191-97 Lack No.184-85,187-90,192,194,196
Author Added Entry:
Thomson,Robert G;
Copy Details:
Acc. No.: TR13580, Full Call No.: NASA TM X-186, Item type: Technical Report , Location: General Stacks,
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