Y 3.N 21/5:6/3364
|
Investigation of effectiveness of large-chord slotted flaps in deflecting propeller slipstreams downward for vertical take-off and low-speed flight / |
1 |
Y 3.N 21/5:6/3365
|
An analysis of accelerations, airspeeds, and gust velocities from three commercial operations of one type of medium-altitude transport airplane / |
2 |
Y 3.N 21/5:6/3366
|
A method for studying the transient blade-flapping behavior of lifting rotors at extreme operating conditions / |
1 |
Y 3.N 21/5:6/3367
|
A dynamic-model study of the effect of added weights and other structural variations on the blade bending strains of an experimental two-blade jet-driven helicopter in hovering and forward flight / |
1 |
Y 3.N 21/5:6/3368
|
Analysis of behavior of simply supported flat plates compressed beyond the buckling load into the plastic range / |
2 |
Y 3.N 21/5:6/3369
|
Minimum-drag bodies of revolution in a nonuniform supersonic flow field / |
1 |
Y 3.N 21/5:6/3370
|
A simplified method for calculating aeroelastic effects on the roll of aircraft / |
1 |
Y 3.N 21/5:6/3371
|
Analysis of accelerations, gust velocities, and airspeeds from operations of a twin-engine transport airplane on a transcontinental route from 1950 to 1952 / |
2 |
Y 3.N 21/5:6/3372
|
Flight measurements of base pressure on bodies of revolution with and without simulated rocket chambers / |
1 |
Y 3.N 21/5:6/3373
|
Theoretical calculations of the pressures, forces, and moments due to various lateral motions acting on thin isolated vertical tails with supersonic leading and trailing edges / |
1 |
Y 3.N 21/5:6/3374
|
Turbulent-heat-transfer measurements at a Mach number of 2.06 / |
1 |
Y 3.N 21/5:6/3375
|
A theory for predicting the flow of real gases in shock tubes with experimental verification / |
1 |
Y 3.N 21/5:6/3376
|
The effect of control stiffness and forward speed on the flutter of a 1/10-scale dynamic model of a two-blade jet-driven helicopter rotor / |
1 |
Y 3.N 21/5:6/3377
|
Flight measurements of the velocity distribution and persistance of the trailing vortices of an airplane / |
1 |
Y 3.N 21/5:6/3378
|
Acoustical treatment for the NACA 8- by 6-foot supersonic propulsion wind tunnel / |
2 |
Y 3.N 21/5:6/3379
|
A survey of background and aircraft noise in communities near airports / |
1 |
Y 3.N 21/5:6/3380
|
Study of effects of microstructure and anisotropy on fatigue of 24S-T4 aluminum alloy / |
1 |
Y 3.N 21/5:6/3381
|
Heat-loss characteristics of hot-wire anemometers at various densities in transonic and supersonic flow / |
1 |
Y 3.N 21/5:6/3382
|
Experiments with a rotating-cylinder viscometer at high shear rates / |
1 |
Y 3.N 21/5:6/3383
|
Investigation of the turbulent boundary layer on a yawed flat plate / |
1 |