Call Number (LC) Title Results
Y 3.N 21/5:6/1700 The Rolling moment due to sideslip of triangular, trapezoidal, and related plan forms in supersonic flow / 1
Y 3.N 21/5:6/1701 Analysis of the performance of a jet engine from characteristics of the components. : 2 - Interaction of the components as determined from engine operation / 1
Y 3.N 21/5:6/1702 Analytical and experimental performance of an explosion-cycle combustion chamber for a jet-propulsion engine / 1
Y 3.N 21/5:6/1703 Downwash and wake behind untapered wings of various aspect ratios and angles of sweep / 1
Y 3.N 21/5:6/1704 Investigation of boundary-layer Reynolds number for transition on an NACA 65₍₂₁₅₎-114 airfoil in the Langley two-dimensional low-turbulence pressure tunnel / 1
Y 3.N 21/5:6/1705 Experimental investigation of the effects of plastic flow in a tension panel with a circular hole / 2
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