000			00410pam a2200133a 44500
082			_aNASA _bCR-2228
100			_aWoodward,F A
245	1		_aAN IMPROVED METHOD FOR THE AERODYNAMIC ANALYSIS OF WING-BODY-TAIL CONFIGURATIONS IN SUBSONIC AND SUPERSONIC FLOW
260			_a _bNasa, Washington, D.C. _c1973
300			_a128
500			_aBound With Nasa Cr-2221-27,2229
964			_gCIRC
997			_aTR12999 C
999			_c398396 _d398396