Call Number (LC) Title Results
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
Y 3.N 21/5:6/4148 Theoretical pressure distributions for several related nonlifting airfoils at high subsonic speeds / 1
Y 3.N 21/5:6/4149 An analysis of the turbulent boundary-layer characteristics on a flat plate with distributed light-gas injection / 1
Y 3.N 21/5:6/4150 Approximations for the thermodynamic and transport properties of high-temperature air / 1
Y 3.N 21/5:6/4151 Correlations among ice measurements, impingement rates, icing conditions, and drag coefficients for unswept NACA 65A004 airfoil / 1
Y 3.N 21/5:6/4152 Laminar boundary layer with heat transfer on a cone at angle of attack in a supersonic stream / 1
Y 3.N 21/5:6/4153 Effect of wall cooling on inlet parameters of a scoop operating in a turbulent boundary layer on a flat or conical surface for Mach numbers 2 to 10 / 1
Y 3.N 21/5:6/4154 Approximate calculation of the compressible turbulent boundary layer with heat transfer and arbitrary pressure gradient / 1
Y 3.N 21/5:6/4155 Aerodynamic effects caused by icing of an unswept NACA 65A004 airfoil / 2
Y 3.N 21/5:6/4156 Effect of initial mixture-temperature on burning velocity of hydrogen-air mixtures with preheating and simulated preburning / 1
Y 3.N 21/5:6/4157 Corrosion resistance of nickel alloys in molten sodium hydroxide / 1
Y 3.N 21/5:6/4158 Accelerations in transport-airplane crashes / 2
Y 3.N 21/5:6/4159 Experimental investigation of turbojet-engine multiple-loop controls for nonafterburning and afterburning modes of engine operation / 1
Y 3.N 21/5:6/4160 Thermal fatigue of ductile materials. : 1 - Effect of variations in the temperature cycle on the thermal-fatigue life of S-816 and Inconel 550 / 1