000			01763 a2200157 4500
005			20230821152331.0
100			_aMayes, H.William
245			_aNASA technical note [D21-30] _bNear-field and far-field noise surverys of solid-fuel rocket engines for a range of nozzle exit pressuress _cNASA
260			_aNational aeronautics and space administration _bNASA _c1959
300			_a32p
500			_aTR8550 : [D-22] Measurement of ground -reaction forces and vertical acceleration at the center of gravity of a transport airplane taxiing over obstacles by James M. Mckay. TR8551 : [D-23] Experimental operating performance of a single-stage annular air ejector by Robert R. Howell. TR8552 : [D-24] Calculation of supersonic flow past bodies supporting shock waves shaped like elliptic cones by Briggs benjamin R. TR8553 : [D25] Large-scale wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing four propellers and blowing flaps by Weiberg, James A. TR8554 : [D-26] Moving-cockpit simulator investigation of the minimum tolerable longitudinal maneuvering stability by Brown, porter B. TR8555 : [D-27] Shielding stagnation surfaces of finite catalytic activity by air injection in hypersonic flight by Chung, paul M. TR8556 : [D-28] A combind water-bromotrifluoromethane crash-fire protection system for A T-56 turbopropeller engine by Campbell, john A. TR8557 : [D-29] Summary of veg and V-G data obtained from 1947 to 1958 by Walker, Walter G. TR8558 : [D-30] Flight investigation of the lift and drag characteristics of a swept-wing multijet transport-type airplance by Tombor Ronald
650			_aNasa technical note
700			_aLandford, H.Hubbard
700			_aHubbard, H. Harvey
942			_cTR
999			_c564259 _d564259