Call Number (LC) Title Results
Y 3.N 21/5:6/3859 Comparison of flight and wind-tunnel measurements of high-speed-airplane stability and control characteristics / 1
Y 3.N 21/5:6/3860 Method for calculating effects of dissociation on flow variables in the relaxation zone behind normal shock waves / 1
Y 3.N 21/5:6/3861 Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90 degrees /
Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° / 		2
Y 3.N 21/5:6/3862 Determination of the structural damping coefficients of six full-scale helicopter rotor blades of different materials and methods of construction / 1
Y 3.N 21/5:6/3863 Wind-tunnel investigation at low speeds to determine the effect of aspect ratio and end plates on a rectangular wing with jet flaps deflected 85 degrees / 1
Y 3.N 21/5:6/3864 Theoretical calculation of the power spectra of the rolling and yawing moments on a wing in random turbulence / 1
Y 3.N 21/5:6/3865 Wind-tunnel investigation of jet-augmented flaps on a rectangular wing to high momentum coefficients / 1
Y 3.N 21/5:6/3866 Fatigue tests on notched and unnotched sheet specimens of 2024-T3 and 7075-T6 aluminum alloys and of SAE 4130 steel with special consideration of the life range from 2 to 10,000 cycles / 1
Y 3.N 21/5:6/3867 Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds. : Taper-ratio series / 1
Y 3.N 21/5:6/3868 Particular solutions for flows at Mach number 1 / 1
Y 3.N 21/5:6/3869 Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition / 1
Y 3.N 21/5:6/3870 Measurement of the longitudinal moment of inertia of a flexible airplane / 1
Y 3.N 21/5:6/3871 Investigation at subsonic speeds of several modifications to the leading-edge region of the NACA 64A010 airfoil section designed to increase maximum lift / 1
Y 3.N 21/5:6/3872 Experimental determination of the range of applicability of the transonic area rule for wings of triangular plan form / 1
Y 3.N 21/5:6/3873 Tables of characteristic functions for solving boundary-value problems of the wave equation with application to supersonic interference / 1
Y 3.N 21/5:6/3874 Experimental and predicted lateral-directional dynamic-response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet / 1
Y 3.N 21/5:6/3875 The similarity rules for second-order subsonic and supersonic flow / 1
Y 3.N 21/5:6/3876 An investigation at low speed of the flow over a simulated flat plate at small angles of attack using pitot-static and hot-wire probes / 1
Y 3.N 21/5:6/3877 On Stokes' stream function in compressible small-disturbance theory / 1
Y 3.N 21/5:6/3878 Theoretical and experimental investigation of random gust loads. : Part 1 - Aerodynamic transfer function of a simple wing configuration in incompressible flow / 1