000			00454pam a2200145a 44500
082			_aNASA _bTN D-3276
100			_aSmall,W J
245	1		_aEFFECT OF GEOMETRIC MODIFICATIONS ON THE MAXIMUM LIFT -DRAG RATIOS OF SLENDER WING-BODY CONFIGURATIONS AT HYPERSONIC SPEEDS
260			_a _bNasa, Washington, D.C. _c1966
300			_a60
500			_aBound With Nasa Tn D-3271-75, 3277-80.
700			_aBertram,M H
964			_gCIRC
997			_aTR11996 C
999			_c396821 _d396821