Call Number (LC) Title Results
Y 3.N 21/5:6/1873 Subsonic two-dimensional-flow conditions near an airfoil determined by static pressures measured at the tunnel wall / 1
Y 3.N 21/5:6/1874 Analysis of altitude compensation systems for aircraft carburetors / 1
Y 3.N 21/5:6/1875 On two-dimensional supersonic flows / 1
Y 3.N 21/5:6/1876 Calculation of the aerodynamic loading of flexible wings of arbitrary plan form and stiffness / 1
Y 3.N 21/5:6/1877 Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60 / 1
Y 3.N 21/5:6/1878 Study of unsteady flow disturbances of large and small amplitudes moving through supersonic or subsonic steady flows / 1
Y 3.N 21/5:6/1879 Critical axial-compressive stress of a curved rectangular panel with a central longitudinal stiffener / 1
Y 3.N 21/5:6/1880 Determination of centrifugal-compressor performance on basis of static-pressure measurements in vaneless diffuser / 1
Y 3.N 21/5:6/1881 Comparison of pitching moments obtained during seaplane landings with values predicted by hydrodynamic impact theory / 1
Y 3.N 21/5:6/1882 Oxidation characteristics of molybdenum disulfide and effect of such oxidation on its role as a solid-film lubricant / 1
Y 3.N 21/5:6/1883 Thermodynamic charts for internal-combustion-engine fluids / 1
Y 3.N 21/5:6/1884 Note on the accuracy of a method for rapidly calculating the increments in velocity about an airfoil due to angle of attack / 1
Y 3.N 21/5:6/1885 Design and calibration of a total-temperature probe for use at supersonic speeds / 1
Y 3.N 21/5:6/1886 Compressive buckling of flat rectangular metalite type sandwich plates with simply supported loaded edges and clamped unloaded edges / 1
Y 3.N 21/5:6/1887 Effect of high shear rate on erosion of common bearing metals / 1
Y 3.N 21/5:6/1888 Response of a helicopter rotor to oscillatory pitch and throttle movements / 1
Y 3.N 21/5:6/1889 Biaxial fatigue strength of 24S-T aluminum alloy / 1
Y 3.N 21/5:6/1890 The effect of torsional flexibility on the rolling characteristics at supersonic speeds of tapered unswept wings / 1
Y 3.N 21/5:6/1891 Elastic buckling of a simply supported plate under a compressive stress that varies linearly in the direction of loading / 1
Y 3.N 21/5:6/1892 Position errors of the service airspeed installations of 10 airplanes / 1