|
Y 3.N 21/5:6/1824
|
Linearized compressible-flow theory for sonic flight speeds / |
1 |
|
Y 3.N 21/5:6/1825
|
Compressive buckling of simply supported plates with longitudinal stiffeners / |
1 |
|
Y 3.N 21/5:6/1826
|
Linear theory of boundary effects in open wind tunnels with finite jet length / |
1 |
|
Y 3.N 21/5:6/1827
|
Matrix methods for calculating cantilever-beam deflections / |
1 |
|
Y 3.N 21/5:6/1828
|
Effect of forebody warp on the hydrodynamic qualities of a hypothetical flying boat having a hull length-beam ratio of 15 / |
1 |
|
Y 3.N 21/5:6/1830
|
Tension properties of aluminum alloys in the presence of stress-raisers. |
1 |
|
Y 3.N 21/5:6/1831
|
Tension properties of aluminum alloys in the presence of stress-raisers. |
1 |
|
Y 3.N 21/5:6/1832
|
Small bending and stretching of sandwich-type shells / |
1 |
|
Y 3.N 21/5:6/1833
|
Notes on the foundations of the theory of small displacements of orthotropic shells / |
1 |
|
Y 3.N 21/5:6/1834
|
The Influence of blade-width distribution on propeller characteristics / |
1 |
|
Y 3.N 21/5:6/1835
|
Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings / |
1 |
|
Y 3.N 21/5:6/1836
|
Initial investigation of carbide-type ceramal of 80-percent titanium carbide plus 20-percent cobalt for use as gas-turbine-blade material / |
1 |
|
Y 3.N 21/5:6/1837
|
Elevated-temperature compressive stress-strain data for 24S-T3 aluminum-alloy sheet and comparisons with extruded 75S-T6 aluminum alloy / |
1 |
|
Y 3.N 21/5:6/1838
|
Dynamometer-stand investigation of a group of mufflers / |
1 |
|
Y 3.N 21/5:6/1839
|
Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip / |
1 |
|
Y 3.N 21/5:6/1840
|
Analysis of properties of foam / |
1 |
|
Y 3.N 21/5:6/1841
|
Quantitative study of variations in concentration of glycerol and Aerosol OT on foaming volume of oil at room temperature / |
1 |
|
Y 3.N 21/5:6/1842
|
Control of foaming by adding known mixtures of pure chemicals / |
1 |
|
Y 3.N 21/5:6/1843
|
Effect of various compounds in use with airplane engines upon foaming of aircraft lubricating oil / |
1 |
|
Y 3.N 21/5:6/1844
|
Surface properties of oils / |
1 |
