000			00572pam a2200145a 44500
082			_aNASA _bTM X-186
100			_aTrussell,Donald H
245	1		_aTESTS 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
260			_a _bNasa, Washington, D.C. _c1960
300			_a33
500			_aBound With Nasa Tm X-182-83,191-97 Lack No.184-85,187-90,192,194,196
700			_aThomson,Robert G
964			_gCIRC
997			_aTR13580 C
999			_c399249 _d399249