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 |