Call Number (LC) Title Results
Y 3.N 21/5:6/4244 On solutions for the transient response of beams / 1
Y 3.N 21/5:6/4245 Flutter analysis of rectangular wings of very low aspect ratio / 1
Y 3.N 21/5:6/4246 Further investigation of fatigue-crack propagation in aluminum-alloy box beams / 1
Y 3.N 21/5:6/4247 Study of ground-reaction forces measured during landing impacts of a large aircraft / 1
Y 3.N 21/5:6/4248 Summary of experimental heat-transfer measurements in turbulent flow for a Mach number range from 0.87 to 5.05 / 1
Y 3.N 21/5:6/4249 A theoretical analysis of the effect of engine angular momentum on longitudinal and directional stability in steady rolling maneuvers / 1
Y 3.N 21/5:6/4250 Effect of the proximity of the wing first-bending frequency and the short-period frequency on the airplane dynamic-response factor / 1
Y 3.N 21/5:6/4251 An experimental investigation of wake effects on hydro-skis / 1
Y 3.N 21/5:6/4252 Experimental investigation of an impulse-type supersonic compressor rotor having a turning of 73 degrees at the mean radius / 1
Y 3.N 21/5:6/4253 Design and tests of a six-stage axial-flow compressor having a tip speed of 550 feet per second and a flat operating characteristic at constant speed / 1
Y 3.N 21/5:6/4254 Flight investigation of effects of retreating-blade stall on bending and torsional moments encountered by a helicopter rotor blade / 1
Y 3.N 21/5:6/4255 Wind-tunnel investigation at low speeds of flight characteristics of a sweptback-wing jet-transport airplane model equipped with an external-flow jet-augmented slotted flap / 1
Y 3.N 21/5:6/4256 Water-impact theory for aircraft equipped with nontrimming hydro-skis mounted on shock struts / 1
Y 3.N 21/5:6/4257 Results of an experimental investigation of small viscous dampers / 1
Y 3.N 21/5:6/4258 A numerical method for evaluating wave drag / 1
Y 3.N 21/5:6/4259 Temperature-pressure-time relations in a closed cryogenic container / 1
Y 3.N 21/5:6/4260 Ground reflection of jet noise / 1
Y 3.N 21/5:6/4261 Acoustic, thrust, and drag characteristics of several full-scale noise suppressors for turbojet engines / 2
Y 3.N 21/5:6/4262 Analysis of turbulent flow and heat transfer on a flat plate at high Mach numbers with variable fluid properties / 1
Y 3.N 21/5:6/4263 Effect of prior air force overtemperature operation on life of J47 buckets evaluated in a sea-level cyclic engine test / 1