Y 3.N 21/5:6/3633
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Analysis of the ultimate strength and optimum proportions of multiweb wing structures / |
1 |
Y 3.N 21/5:6/3634
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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
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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
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The accuracy of the substitute-stringer approach for determining the bending frequencies of multistringer box beams / |
2 |
Y 3.N 21/5:6/3637
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Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes / |
1 |
Y 3.N 21/5:6/3638
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On panel flutter and divergence of infinitely long unstiffened and ring-stiffened thin-walled circular cylinders / |
1 |
Y 3.N 21/5:6/3639
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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
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A method for deflection analysis of thin low-aspect-ratio wings / |
1 |
Y 3.N 21/5:6/3641
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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
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Effect of shallow water on the hydrodynamic characteristics of a flat-bottom planing surface / |
1 |
Y 3.N 21/5:6/3643
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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
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Lift and moment coefficients for an oscillating rectangular wing-aileron configuration in supersonic flow / |
1 |
Y 3.N 21/5:6/3645
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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
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A theory for the elastic deflections of plates integrally stiffened on one side / |
1 |
Y 3.N 21/5:6/3647
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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
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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
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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
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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
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Cross flows in laminar incompressible boundary layers / |
1 |
Y 3.N 21/5:6/3652
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Experimental investigation of air-flow uniformity and pressure level on wire cloth for transpiration-cooling applications / |
1 |