Call Number (LC) Title Results
Y 3.N 21/5:6/4266 Studies of OH, CO, CH, and C2 radiation from laminar and turbulent propane-air and ethylene-air flames / 1
Y 3.N 21/5:6/4267 Preliminary survey of propulsion using chemical energy stored in the upper atmosphere / 1
Y 3.N 21/5:6/4268 Droplet impingement and ingestion by supersonic nose inlet in subsonic tunnel conditions / 1
Y 3.N 21/5:6/4269 Transonic drag of several jet-noise suppressors / 1
Y 3.N 21/5:6/4270 A performance analysis of methods for handling excess inlet flow at supersonic speeds / 1
Y 3.N 21/5:6/4271 Maximum theoretical tangential velocity component possible from straight-back converging and converging-diverging stators at supercritical pressure ratios / 1
Y 3.N 21/5:6/4272 Use of the Coanda effect for obtaining jet deflection and lift with a single flat-plate deflection surface / 1
Y 3.N 21/5:6/4273 On pairs of solutions of a class of internal viscous flow problems with body forces / 1
Y 3.N 21/5:6/4274 Measurement of the effect of an axial magnetic field on the Reynolds number of transition in mercury flowing through a glass tube / 1
Y 3.N 21/5:6/4275 Dynamic stability of vehicles traversing ascending or descending paths through the atmosphere / 1
Y 3.N 21/5:6/4276 An approximate analytical method for studying entry into planetary atmospheres / 1
Y 3.N 21/5:6/4277 A body modification to reduce drag due to wedge angle of wing with unswept tailing edge / 1
Y 3.N 21/5:6/4278 Application of statistical theory to beam-rider guidance in the presence of noise. : 2 - Modified Wiener filter theory / 1
Y 3.N 21/5:6/4279 Effects of fixing transitiion on the transonic aerodynamic characteristics of a wing-body configuration at Reynolds numbers from 2.4 to 12 million / 1
Y 3.N 21/5:6/4280 Pressure distributions at transonic speeds for slender bodies having various axial locations of maximum diameter / 1
Y 3.N 21/5:6/4281 Second-order slender-body theory : Axisymmetric flow / 1
Y 3.N 21/5:6/4282 Boundary-layer stability diagrams for electrically conducting fluids in the presence of a magnetic field / 1
Y 3.N 21/5:6/4283 Full-scale wind-tunnel tests of a 35 degree sweptback-wing airplane with blowing from the shroud ahead of the trailing-edge flaps / 1
Y 3.N 21/5:6/4284 Cumulative fatigue damage at elevated temperature / 1
Y 3.N 21/5:6/4285 Transgranular and intergranular fractures of ingot iron during creep / 1