Call Number (LC) Title Results
Y 3.N 21/5:6/2853 A study of the application of power-spectral methods of generalized harmonic analysis to gust loads on airplanes / 1
Y 3.N 21/5:6/2854 Average skin-friction drag coefficients from tank tests of a parabolic body of revolution (NACA RM-10) / 1
Y 3.N 21/5:6/2855 General correlation of temperature profiles downstream of a heated air jet directed at various angles to air stream / 1
Y 3.N 21/5:6/2856 Estimated power reduction by water injection in a nonreturn supersonic wind tunnel / 1
Y 3.N 21/5:6/2857 A theoretical method of analyzing the effects of yaw-damper dynamics on the stability of an aircraft equipped with a second-order yaw damper / 1
Y 3.N 21/5:6/2858 Supersonic wave drag of nonlifting delta wings with linearly varying thickness ratio / 1
Y 3.N 21/5:6/2859 The Langley 2,000-horsepower propeller dynamometer and tests at high speed of an NACA 10-(3)(08)-03 two-blade propeller / 1
Y 3.N 21/5:6/2860 Interaction between a supersonic stream and a parallel subsonic stream bounded by fluid at rest / 1
Y 3.N 21/5:6/2861 Analytical investigation of icing limit for diamond-shaped airfoil in transonic and supersonic flow / 1
Y 3.N 21/5:6/2862 Influence of nonmartensitic transformation products on mechanical properties of tempered martensite / 1
Y 3.N 21/5:6/2863 Laminar natural-convection flow and heat transfer of fluids with and without heat sources in channels with constant wall temperatures / 1
Y 3.N 21/5:6/2864 Convection of a pattern of vorticity through a shock wave / 1
Y 3.N 21/5:6/2865 Investigation of gases evolved during firing of vitreous coatings on steel / 1
Y 3.N 21/5:6/2866 Icing protection for a turboject transport airplane: heating requirements, methods of protection, and performance penalties / 1
Y 3.N 21/5:6/2867 Heat and momentum transfer between a spherical particle and air streams / 1
Y 3.N 21/5:6/2868 Reflection of a weak shock wave from a boundary layer along a flat plate. : 1 - Interaction of weak shock waves with laminar and turbulent boundary layers analyzed by momentum-integral method / 1
Y 3.N 21/5:6/2869 Reflection of a weak shock wave from a boundary layer along a flat plate. : 2 - Interaction of oblique shock wave with a laminar boundary layer analyzed by differential-equation method / 1
Y 3.N 21/5:6/2870 Power-off flare-up tests of a model helicopter rotor in vertical autorotation / 1
Y 3.N 21/5:6/2871 Experimental investigation of loss in an annular cascade of turbine-nozzle blades of free vortex design / 1
Y 3.N 21/5:6/2872 The effect of initial curvature on the strength of an inelastic column / 1