Call Number (LC) Title Results
Y 3.N 21/5:6/1706 Stability derivatives of thin rectangular wings at supersonic speeds. : Wing diagonals ahead of tip Mach lines / 1
Y 3.N 21/5:6/1707 Effect of Reynolds number in the turbulent-flow range on flame speeds of bunsen-burner flames / 1
Y 3.N 21/5:6/1708 Theoretical characteristics in supersonic flow of constant-chord partial-span control surfaces on rectangular wings having finite thickness / 1
Y 3.N 21/5:6/1709 Investigation of the effects of a nacelle on the aerodynamic characteristics of a swept wing and the effects of sweep on a wing alone / 1
Y 3.N 21/5:6/1710 Minimum-weight design of simply supported transversely stiffened plates under compression / 1
Y 3.N 21/5:6/1711 Approximate relations for hinge-moment parameters of control surfaces on swept wings at low Mach numbers / 1
Y 3.N 21/5:6/1712 Analytical method of determining transmission of particles and radiation through great thickness of matter / 1
Y 3.N 21/5:6/1713 Experimental study of effect of vaneless-diffuser diameter on diffuser performance / 1
Y 3.N 21/5:6/1714 Plate compressive strength of FS-1h magnesium-alloy sheet and a maximum-strength formula for magnesium-alloy and aluminum-alloy formed sections / 1
Y 3.N 21/5:6/1715 Mollier diagrams for air saturated with water vapor at low temperatures / 1
Y 3.N 21/5:6/1716 Tables of hypergeometric functions for use in compressible-flow theory / 1
Y 3.N 21/5:6/1717 Gust-tunnel investigation of a 45 degree sweptforward-wing model / 1
Y 3.N 21/5:6/1718 Influence of leading-edge suction on lift-drag ratios of wings at supersonic speeds / 1
Y 3.N 21/5:6/1719 Flight measurements of buffeting tail loads / 1
Y 3.N 21/5:6/1720 Friction at high sliding velocities on surfaces lubricated with sulfur as an additive / 1
Y 3.N 21/5:6/1721 Calculation of the effect of thrust-axis inclination on propeller disk loading and comparison with flight measurements / 1
Y 3.N 21/5:6/1722 Prediction of the effects of propeller operation on the static longitudinal stability of single-engine tractor monoplanes with flaps retracted / 1
Y 3.N 21/5:6/1723 A theoretical investigation of the effect of yawing moment due to rolling on lateral oscillatory stability / 1
Y 3.N 21/5:6/1724 A study of skin temperatures of conical bodies in supersonic flight / 1
Y 3.N 21/5:6/1725 Determination of transient skin temperature of conical bodies during short-time, high-speed flight / 1