000			00540pam a2200145a 44500
082			_aNASA _bTN D-1959 -
100			_aGoldberg,Theodore J
245	1		_aEFFECTS OF ROUNDING CORNERS AND LEADING EDGES ON THE WINDWARD-SURFACE PRESSURE OF A DELTA WING SWEPT 65(DG) AT A MACH NUMBER OF 5.96 AT ANGLES OF ATTACK FROM 65(DG) TO 115(DG)AND ANGLES OF ROLL FROM..
260			_a _bNasa, Washington, D.C. _c1963
300			_a34
500			_aBound With Nasa Tn D-1951-1960
700			_aBlanchard,Doris K
964			_gCIRC
997			_aTR8715 C
999			_c394384 _d394384