Call Number (LC) | Title | Results |
---|---|---|
Y 3.N 21/5:6/869 | Summary of results of tests made by aluminum research laboratories of spot-welded joints and structural elements / | 2 |
Y 3.N 21/5:6/870 |
Stress analysis of monocoque fuselage bulkheads by the photoelectric method / Stress analysis of monocoque fuselage bulkheads by the photoelastic method / |
2 |
Y 3.N 21/5:6/871 | Stability of elastically supported columns / | 2 |
Y 3.N 21/5:6/872 | Torsion test of a monocoque box / | 2 |
Y 3.N 21/5:6/873 | Bending tests of a monocoque box / | 2 |
Y 3.N 21/5:6/874 | Curing of resin-wood combinations by high-frequency heating / | 2 |
Y 3.N 21/5:6/875 |
A Rosette Strain Computer, Dec. 1942. A Rosette strain computer / |
2 |
Y 3.N 21/5:6/876 | The Limiting useful deflections of corrugated metal diaphragms / | 1 |
Y 3.N 21/5:6/877 | An Exploration of the longitudinal tensile and compressive properties throughout an extruded shape of 24S-T aluminum alloy / | 1 |
Y 3.N 21/5:6/878 | Effect of fillers and of mixing procedure on the strength of plastic materials / | 1 |
Y 3.N 21/5:6/879 | Torsional strength of aluminum-alloy round tubing / | 1 |
Y 3.N 21/5:6/880 | Methods of measurement of high air velocities by the hot-wire method / | 1 |
Y 3.N 21/5:6/881 | A hot-wire circuit with very small time lag / | 1 |
Y 3.N 21/5:6/882 | Tests of flat panels with four types of stiffeners / | 1 |
Y 3.N 21/5:6/883 | Tests of aluminum-alloy stiffened-sheet specimens cut from an airplane wing / | 1 |
Y 3.N 21/5:6/884 | Large-deflection theory for end compression of long rectangular plates rigidly clamped along two edges / | 1 |
Y 3.N 21/5:6/885 | Torsion tests of 24S-T aluminum-alloy noncircular bar and tubing / | 1 |
Y 3.N 21/5:6/886 | Torsional elastic properties of 18:8 chromium-nickel steel as affected by plastic deformation and by heat treatment / | 1 |
Y 3.N 21/5:6/887 | A Portable calibrator for dynamic strain gages / | 1 |
Y 3.N 21/5:6/888 | Torsion of flanged members with cross sections restrained against warping / | 1 |