Call Number (LC) Title Results
Y 3.N 21/5:6/3633 Analysis of the ultimate strength and optimum proportions of multiweb wing structures / 1
Y 3.N 21/5:6/3634 Calculations of the rate of thermal dissociation of air behind normal shock waves at Mach numbers of 10, 12, 14 / 1
Y 3.N 21/5:6/3635 Analytical study of modification to the autopilot of a fighter airplane in order to reduce the response to side gusts / 1
Y 3.N 21/5:6/3636 The accuracy of the substitute-stringer approach for determining the bending frequencies of multistringer box beams / 2
Y 3.N 21/5:6/3637 Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes / 1
Y 3.N 21/5:6/3638 On panel flutter and divergence of infinitely long unstiffened and ring-stiffened thin-walled circular cylinders / 1
Y 3.N 21/5:6/3639 Approximate indicial lift functions for several wings of finite span in incompressible flow as obtained from oscillatory lift coefficients / 1
Y 3.N 21/5:6/3640 A method for deflection analysis of thin low-aspect-ratio wings / 1
Y 3.N 21/5:6/3641 Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack : Subsonic, transonic, and supersonic speeds / 1
Y 3.N 21/5:6/3642 Effect of shallow water on the hydrodynamic characteristics of a flat-bottom planing surface / 1
Y 3.N 21/5:6/3643 Measurement of aerodynamic forces for various mean angles of attack on an airfoil oscillating in pitch and on two finite-span wings oscillating in bending with emphasis on damping in the stall / 1
Y 3.N 21/5:6/3644 Lift and moment coefficients for an oscillating rectangular wing-aileron configuration in supersonic flow / 1
Y 3.N 21/5:6/3645 Wind-tunnel investigation of effects of fuselage cross-sectional shape, fuselage bend, and vertical-tail size on directional characteristics of nonoverlap-type helicopter fuselage models without rotors / 1
Y 3.N 21/5:6/3646 A theory for the elastic deflections of plates integrally stiffened on one side / 1
Y 3.N 21/5:6/3647 Investigation of the compressive strength and creep lifetime of 2024-T aluminum-alloy skin-stringer panels at elevated temperatures / 1
Y 3.N 21/5:6/3648 Investigation of boundary-layer transition on 10 degree cone in Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.41, 1.61, and 2.01 / 1
Y 3.N 21/5:6/3649 Static longitudinal and lateral stability characteristics at low speed of unswept-midwing models having wings with an aspect ratio of 2, 4, or 6 / 1
Y 3.N 21/5:6/3650 Results of a flight investigation to determine the zero-lift drag characteristics of a 60 degree delta wing with NACA 65-006 airfoil section and various double-wedge sections at Mach numbers from 0.7 to 1.6 / 1
Y 3.N 21/5:6/3651 Cross flows in laminar incompressible boundary layers / 1
Y 3.N 21/5:6/3652 Experimental investigation of air-flow uniformity and pressure level on wire cloth for transpiration-cooling applications / 1