Call Number (LC) Title Results
Y 3.N 21/5:6/1914 Oxidation of titanium carbide base ceramals containing molybdenum, tungsten, and cobalt / 1
Y 3.N 21/5:6/1915 Elevated-temperature properties of several titanium carbide base ceramals / 1
Y 3.N 21/5:6/1916 The effects of sideslip, aspect ratio, and mach number on the lift and pitching moment of triangular, trapezoidal, and related plan forms in supersonic flow / 1
Y 3.N 21/5:6/1917 An analysis of the relation between horizontal temperature variations and maximum effective gust velocities in thunderstorms / 1
Y 3.N 21/5:6/1918 Correlation of physical properties of ceramic materials with resistance to fracture by thermal shock / 1
Y 3.N 21/5:6/1919 Analytical method for determining transmission and absorption of time-dependent radiation through thick absorbers. 1
Y 3.N 21/5:6/1920 Preliminary investigation of needle bearings of 1 1/8-inch pitch diameter at speeds to 17,000 rpm / 1
Y 3.N 21/5:6/1921 Approximate method for predicting form and location of detached shock waves ahead of plane or axially symmetric bodies / 1
Y 3.N 21/5:6/1922 Two-dimensional investigation of five related NACA airfoil sections designed for rotating-wing aircraft / 1
Y 3.N 21/5:6/1923 Boundary-layer and stalling characteristics of the NACA 64A006 airfoil section / 1
Y 3.N 21/5:6/1924 Estimation of the damping in roll of wings through the normal flight range of lift coefficient / 1
Y 3.N 21/5:6/1925 Line-vortex theory for calculation of supersonic downwash / 1
Y 3.N 21/5:6/1926 The application of the statistical theory of extreme values to gust-load problems / 1
Y 3.N 21/5:6/1927 Generalization of turbojet-engine performance in terms of pumping characteristics / 1
Y 3.N 21/5:6/1928 Critical combinations of shear and direct axial stress for curved rectangular panels
Critical combinations of shear and direct axial stress for curved rectangular panels / 		2
Y 3.N 21/5:6/1929 On the stability of the free laminar boundary layer between parallel streams / 1
Y 3.N 21/5:6/1930 An analysis of the effect of lift-drag ratio and stalling speed on landing-flare characteristics / 1
Y 3.N 21/5:6/1931 Design method for two-dimensional channels for compressible flow with application to high-solidity cascades / 1
Y 3.N 21/5:6/1932 Two-dimensional compressible flow in centrifugal compressors with straight blades / 1
Y 3.N 21/5:6/1933 Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65-series wings equipped with full-span slotted flaps / 1