Call Number (LC) Title Results
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
Y 3.N 21/5:6/1934 Low-speed experimental investigation of a thin, faired, double-wedge airfoil section with nose and trailing-edge flaps / 1
Y 3.N 21/5:6/1935 Methods for determining frequency response of engines and control systems from transient data / 1
Y 3.N 21/5:6/1936 A flight determination of the tolerable range of effective dihedral on a conventional fighter airplane / 1
Y 3.N 21/5:6/1937 A flight investigation of the effects of compressibility on applied gust loads / 1
Y 3.N 21/5:6/1938 Mechanisms of failure of high nickel-alloy turbojet combustion liners / 1
Y 3.N 21/5:6/1939 The effects of aerodynamic brakes upon the speed characteristics of airplanes / 1
Y 3.N 21/5:6/1940 Fundamental effects of aging on creep properties of solution-treated low-carbon N-155 alloy / 1
Y 3.N 21/5:6/1941 Attainable circulation of airfoils in cascade / 1
Y 3.N 21/5:6/1942 The effect of wall friction on the strength of shock waves in tubes and hydraulic jumps in channels / 1
Y 3.N 21/5:6/1943 Theoretical relations between the stability derivatives of a wing in direct and in reverse supersonic flow / 1
Y 3.N 21/5:6/1944 The reversibility theorem for thin airfoils in subsonic and supersonic flow / 1