Call Number (LC) Title Results
Y 3.N 21/5:6/3956 Lift and moment responses to penetration of sharp-edged traveling gusts, with application to penetration of weak blast waves / 1
Y 3.N 21/5:6/3957 Some effects of tail height and wing plan form on the static longitudinal stability characteristics of a small-scale model at high subsonic speeds / 1
Y 3.N 21/5:6/3958 Analysis of static aeroelastic behavior of low-aspect-ratio rectangular wings / 1
Y 3.N 21/5:6/3959 Cascade investigation of a related series of 6-percent-thick guide-vane profiles and design charts / 1
Y 3.N 21/5:6/3960 Expected number of maxima and minima of a stationary random process with non-Gaussian frequency distribution / 1
Y 3.N 21/5:6/3961 Effects of fuselage nose length and a canopy on the static longitudinal and lateral stability characteristics of 45 degree sweptback airplane models having fuselages with square cross sections / 1
Y 3.N 21/5:6/3962 The erosion of meteors and high-speed vehicles in the upper atmosphere / 1
Y 3.N 21/5:6/3963 A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry / 1
Y 3.N 21/5:6/3964 The linearized subsonic flow about symmetrical nonlifting wing-body combinations / 1
Y 3.N 21/5:6/3965 Measurements of the nonlinear variation with temperature of heat-transfer rate from hot wires in transonic and supersonic flow / 1
Y 3.N 21/5:6/3966 Theoretical investigation of the effects of configuration changes on the center-of-pressure shift of a body-wing-tail combination due to angle of attack and Mach number at transonic and supersonic speeds / 1
Y 3.N 21/5:6/3967 Characteristics of a 40 degree cone for measuring Mach number, total pressure, and flow angles at supersonic speeds / 1
Y 3.N 21/5:6/3968 The application of matrix methods to coordinate transformations occurring in systems studies involving large motions of aircraft / 1
Y 3.N 21/5:6/3969 A theoretical study of the effect of upstream transpiration cooling on the heat-transfer and skin-friction characteristics of a compressible, laminar boundary layer / 1
Y 3.N 21/5:6/3970 Thin airfoil theory based on approximate solution of the transonic flow equation / 1
Y 3.N 21/5:6/3971 On flow of electrically conducting fluids over a flat plate in the presence of a transverse magnetic field / 1
Y 3.N 21/5:6/3972 Effect of frequency and temperature on fatigue of metals / 1
Y 3.N 21/5:6/3973 Origin and prevention of crash fires in turbojet aircraft / 1
Y 3.N 21/5:6/3974 Full-scale investigation of several jet-engine noise-reduction nozzles / 1
Y 3.N 21/5:6/3975 Investigation of a full-scale, cascade-type thrust reverser / 1