Call Number (LC) Title Results
Y 3.N 21/5:6/3538 Summary of derived gust velocities obtained from measurements within thunderstorms / 1
Y 3.N 21/5:6/3539 Some effects of system nonlinearities in the problem of aircraft flutter / 1
Y 3.N 21/5:6/3540 A reevaluation of gust-load statistics for applications in spectral calculations / 1
Y 3.N 21/5:6/3541 A method for obtaining statistical data on airline vertical velocity at ground contact from measurements of center-of-gravity acceleration / 1
Y 3.N 21/5:6/3542 Analysis of stresses in the plastic range around a circular hole in a plate subjected to uniaxial tension / 1
Y 3.N 21/5:6/3543 Some effects of fuselage flexibility on longitudinal stability and control / 1
Y 3.N 21/5:6/3544 Comparison between theoretical and experimental stresses in circular semimonocoque cylinders with rectangular cutouts / 1
Y 3.N 21/5:6/3545 Investigation of the effect of short fixed diffusers on starting blowdown jets in the Mach number range from 2.7 to 4.5 / 1
Y 3.N 21/5:6/3546 Exploratory investigation of boundary-layer transition on a hollow cylinder at a Mach number of 6.9 / 1
Y 3.N 21/5:6/3547 Aerodynamic characteristics of a small-scale shrouded propeller at angles of attack from 0 to 90 degrees / 1
Y 3.N 21/5:6/3548 Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift / 1
Y 3.N 21/5:6/3549 Flight investigation at Mach numbers from 0.8 to 1.5 to determine the effects of nose bluntness on the total drag of two fin-stabilized bodies of revolution / 1
Y 3.N 21/5:6/3550 Measurements of the effect of trailing-edge thickness on the zero-lift drag of thin low-aspect-ratio wings / 1
Y 3.N 21/5:6/3551 Experimental investigation at low speed of effects of fuselage cross section on static longitudinal and lateral stability characteristics of models having 0 and 45 degree sweptback surfaces / 1
Y 3.N 21/5:6/3552 Investigation of the compressive strength and creep lifetime of 2024-T3 aluminum-alloy plates at elevated temperatures / 1
Y 3.N 21/5:6/3553 Compressive crippling of structural sections / 1
Y 3.N 21/5:6/3554 A preliminary investigation of the effects of frequency and amplitude on the rolling derivatives of an unswept-wing model oscillating in roll / 1
Y 3.N 21/5:6/3555 A method for calculating the contour of bodies of revolution with a prescribed pressure gradient at supersonic speed with experimental verification / 1
Y 3.N 21/5:6/3556 Grain-boundary behavior in creep of aluminum bicrystals / 1
Y 3.N 21/5:6/3557 A theoretical analysis of the field of a random noise source above an infinite plane / 1