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
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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
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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 |
Y 3.N 21/5:6/1893
|
Effect of centrifugal force on flutter of uniform cantilever beam at subsonic speeds with application to compressor and turbine blades / |
1 |
Y 3.N 21/5:6/1894
|
Boundary-layer and stalling characteristics of the NACA 63-009 airfoil section / |
1 |
Y 3.N 21/5:6/1895
|
Effect of aspect ratio on undamped torsional oscillations of a thin rectangular wing in supersonic flow / |
1 |
Y 3.N 21/5:6/1896
|
Improvement of accuracy of balanced-pressure indicators and development of an indicator calibrating machine / |
1 |
Y 3.N 21/5:6/1897
|
Aerodynamic properties of cruciform-wing and body combinations at subsonic, transonic, and supersonic speeds / |
2 |
Y 3.N 21/5:6/1898
|
Effect of a 90° cross wind on the take-off distance of a light airplane equipped with a cross-wind landing gear / |
1 |
Y 3.N 21/5:6/1899
|
Velocity distributions on arbitrary airfoils in closed tunnels by conformal mapping / |
1 |
Y 3.N 21/5:6/1900
|
Preliminary investigation of the use of afterglow for visualizing low-density compressible flows / |
1 |