Call Number (LC) Title Results
Y 3.N 21/5:6/3292 Influence of exposed area on stress-corrosion cracking of 24S aluminum alloy / 1
Y 3.N 21/5:6/3293 Cumulative fatigue damage of axially loaded Alclad 75S-T6 and Alclad 24S-T3 aluminum-alloy sheet / 1
Y 3.N 21/5:6/3294 Friction study of aircraft tire material on concrete / 1
Y 3.N 21/5:6/3295 Effect of pressure on thermal conductance of contact joints / 1
Y 3.N 21/5:6/3296 Separation, stability, and other properties of compressible boundary layer with pressure gradient and heat transfer / 1
Y 3.N 21/5:6/3297 Effect of oxygen content of furnace atmosphere on adherence of vitreous coatings on iron / 1
Y 3.N 21/5:6/3298 A low-density wind-tunnel study of shock-wave structure and relaxation phenomena in gases / 1
Y 3.N 21/5:6/3299 Maximum theorems and reflections of simple waves / 1
Y 3.N 21/5:6/3300 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 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 Liquefaction of air in the Langley 11-inch hypersonic tunnel / 1
Y 3.N 21/5:6/3303 Turbulent-heat-transfer measurements at a Mach number of 3.03 / 1
Y 3.N 21/5:6/3304 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 Some measurements and power spectra of runway roughness / 1
Y 3.N 21/5:6/3306 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 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 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 Mechanical properties at room temperature of four cermets of tungsten carbide with cobalt binder / 1
Y 3.N 21/5:6/3310 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 Description and analysis of a rocket-vehicle experiment on flutter involving wing deformation and body motions / 1