Call Number (LC) Title Results
Y 3.N 21/5:6/3809 A method for calculation of free-space sound pressures near a propeller in flight including considerations of the chordwise blade loading / 1
Y 3.N 21/5:6/3810 Charts for estimating the hovering endurance of a helicopter / 1
Y 3.N 21/5:6/3811 Charts adapted from Van Driest's turbulent flat-plate theory for determining values of turbulent aerodyamic friction and heat-transfer coefficients / 1
Y 3.N 21/5:6/3812 Flight investigation of the stability and control characteristics of a vertically rising airplane research model with swept or unswept wings and X- or +-tails / 1
Y 3.N 21/5:6/3813 Comparison of theoretical stresses and deflections of multicell wings with experimental results obtained from plastic models / 1
Y 3.N 21/5:6/3814 Effects of vertical fins near the nose of the fuselage on the directional and damping-in-yaw stability derivatives of an airplane model under steady-state and oscillatory conditions / 1
Y 3.N 21/5:6/3815 On slender-body theory and the area rule at transonic speeds / 1
Y 3.N 21/5:6/3816 Static strength of aluminum-alloy specimens containing fatigue cracks / 1
Y 3.N 21/5:6/3817 Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading / 1
Y 3.N 21/5:6/3818 Wind-tunnel investigation to determine the horizontal- and vertical-tail contributions to the static lateral stability characteristics of a complete-model swept-wing configuration at high subsonic speeds / 1
Y 3.N 21/5:6/3819 Base pressure at supersonic speeds on two-dimensional airfoils and on bodies of revolution with and without fins having turbulent boundary layers / 1
Y 3.N 21/5:6/3820 Some observations on maximum pressure rise across shocks without boundary-layer separation on airfoils at transonic speeds / 1
Y 3.N 21/5:6/3821 Flight techniques for determining airplane drag at high Mach numbers / 1
Y 3.N 21/5:6/3822 Some measurements of aerodynamic forces and moments at subsonic speeds on a wing-tank configuration oscillating in pitch about the wing midchord / 1
Y 3.N 21/5:6/3823 Investigation of rotating stall in a single-stage axial compressor / 1
Y 3.N 21/5:6/3824 Effect of an interface on transient temperature distribution in composite aircraaft joints / 1
Y 3.N 21/5:6/3825 Comparison of mechanical properties of flat sheets, molded shapes, and postformed shapes of cotton-fabric phenolic laminates / 1
Y 3.N 21/5:6/3826 Investigation of a nonlinear control system / 1
Y 3.N 21/5:6/3827 Experimental investigation of a lightweight rocket chamber / 1
Y 3.N 21/5:6/3828 Investigation of the NiA1 phase of nickel-aluminum alloys / 1