Call Number (LC) Title Results
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