Call Number (LC) Title Results
Y 3.N 21/5:6/4128 A thermocouple subcarrier oscillator for telemetering temperatures from pilotless aircraft / 1
Y 3.N 21/5:6/4129 Analysis of operational airline data to show the effects of airborne weather radar on the gust loads and operating practices of twin-engine short-haul transport airplanes / 1
Y 3.N 21/5:6/4130 NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results / 1
Y 3.N 21/5:6/4131 Transition-flight investigation of a four-engine-transport vertical-take-off airplane model utilizing a large flap and extensible vanes for redirecting the propeller silpstream / 1
Y 3.N 21/5:6/4132 Fatigue investigation of full-scale transport-airplane wings. : Variable-amplitude test with a gust-loads spectrum / 1
Y 3.N 21/5:6/4133 Boundary-layer displacement effects in air at Mach numbers of 6.8 and 9.6 / 1
Y 3.N 21/5:6/4134 Stall propagation in a cascade of airfoils / 1
Y 3.N 21/5:6/4135 Influence of solid-body rotation on screen-produced turbulence / 1
Y 3.N 21/5:6/4136 Theoretical investigation of subsonic oscillatory blade-row aerodynamics / 1
Y 3.N 21/5:6/4137 Fatigue behavior of aircraft structural beams / 1
Y 3.N 21/5:6/4138 Creep deformation patterns of joints under bearing and tensile loads / 1
Y 3.N 21/5:6/4139 Wall pressure fluctuations in a turbulent boundary layer / 1
Y 3.N 21/5:6/4140 Turbulent shearing stress in the boundary layer of yawed flat plates / 1
Y 3.N 21/5:6/4141 The useful heat capacity of several materials for ballistic nose-cone construction / 1
Y 3.N 21/5:6/4142 Effects of leading-edge blunting on the local heat transfer and pressure distributions over flat plates in supersonic flow / 1
Y 3.N 21/5:6/4143 Development of a piston-compressor type light-gas gun for the launching of free-flight models at high velocity / 1
Y 3.N 21/5:6/4144 Effect of oxygen recombination on one-dimensional flow at high Mach numbers / 1
Y 3.N 21/5:6/4145 An analysis of the optimization of a beam rider missile system / 1
Y 3.N 21/5:6/4146 Contribution of the wing panels to the forces and moments of supersonic wing-body combinations at combined angles / 1
Y 3.N 21/5:6/4147 Measured and predicted dynamic response characteristics of a flexible airplane to elevator control over a frequency range including three structural modes / 1