Y 3.N 21/5:6/3292
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Influence of exposed area on stress-corrosion cracking of 24S aluminum alloy / |
1 |
Y 3.N 21/5:6/3293
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Cumulative fatigue damage of axially loaded Alclad 75S-T6 and Alclad 24S-T3 aluminum-alloy sheet / |
1 |
Y 3.N 21/5:6/3294
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Friction study of aircraft tire material on concrete / |
1 |
Y 3.N 21/5:6/3295
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Effect of pressure on thermal conductance of contact joints / |
1 |
Y 3.N 21/5:6/3296
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Separation, stability, and other properties of compressible boundary layer with pressure gradient and heat transfer / |
1 |
Y 3.N 21/5:6/3297
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Effect of oxygen content of furnace atmosphere on adherence of vitreous coatings on iron / |
1 |
Y 3.N 21/5:6/3298
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A low-density wind-tunnel study of shock-wave structure and relaxation phenomena in gases / |
1 |
Y 3.N 21/5:6/3299
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Maximum theorems and reflections of simple waves / |
1 |
Y 3.N 21/5:6/3300
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Investigation of lift, drag, and pitching moment of a 60 degree delta-wing-body combination (AGARD Calibration Model B) in the Langley 9-inch supersonic tunnel / |
1 |
Y 3.N 21/5:6/3301
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Comparison of flutter calculations using various aerodynamic coefficients with experimental results for some rectangular cantilever wings at Mach number 1.3 / |
1 |
Y 3.N 21/5:6/3302
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Liquefaction of air in the Langley 11-inch hypersonic tunnel / |
1 |
Y 3.N 21/5:6/3303
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Turbulent-heat-transfer measurements at a Mach number of 3.03 / |
1 |
Y 3.N 21/5:6/3304
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Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90° / |
1 |
Y 3.N 21/5:6/3305
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Some measurements and power spectra of runway roughness / |
1 |
Y 3.N 21/5:6/3306
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An investigation of a lifing 10-percent-thick symmetrical double-wedge airfoil at Mach numbers up to 1 / |
1 |
Y 3.N 21/5:6/3307
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An investigation of a wing-propeller configuration employing large-chord plain flaps and large-diameter propellers for low-speed flight and vertical take-off / |
1 |
Y 3.N 21/5:6/3308
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An exploratory investigation of some types of aeroelastic instability of open and closed bodies of revolution mounted on slender struts / |
1 |
Y 3.N 21/5:6/3309
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Mechanical properties at room temperature of four cermets of tungsten carbide with cobalt binder / |
1 |
Y 3.N 21/5:6/3310
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Investigation of static strength and creep behavior of an aluminum-alloy multiweb box beam at elevated temperatures / |
1 |
Y 3.N 21/5:6/3311
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Description and analysis of a rocket-vehicle experiment on flutter involving wing deformation and body motions / |
1 |