000			00485pam a2200133a 44500
082			_aNASA _bMEMO 5-28-59L
100			_aGoldberg,Theodore J
245	1		_aINVESTIGATION ON THE USE OF A FREELY ROTATING ROTOR AT THE COWL FACE OF A SUPERSONIC CONICAL INLET TO REDUCE INLET FLOW DISTORTION
260			_a _bNasa, Washington, D.C. _c1959
500			_aBound With Nasa Memo 5-12-59l-5-26-59l Lack No.14-17, 19, 21-22, 27
700			_aBoxer,Emanuel
964			_gCIRC
997			_aTR7412 C
999			_c402221 _d402221