| Call Number (LC) | Title | Results |
|---|---|---|
| Y 3.N 21/5:6/832 | Relief of residual stress in streamline tie rods by heat treatment / | 2 |
| Y 3.N 21/5:6/833 | Ultimate stresses developed by 24S-T sheet in incomplete diagonal tension / | 2 |
| Y 3.N 21/5:6/834 | The calculation of span load distributions on swept-back wings / | 2 |
| Y 3.N 21/5:6/835 | Analysis of ground effect on the lifting airscrew / | 2 |
| Y 3.N 21/5:6/836 |
Hydrodynamic tests of a 1/10-size model of the hull of the Latécoè̀re 521 flying boat - NACA model 83 / Hydrodynamic tests of a 1/10-size model of the hull of the Latecoere 521 flying boat - NACA model 83 / |
2 |
| Y 3.N 21/5:6/837 | Notes on the stability and control of tailless airplanes / | 2 |
| Y 3.N 21/5:6/838 |
The tracer gas method of determining the charging efficiency of two-stroke-cycle diesel engines / The Tracer gas method of determining the charging efficiency of two-stroke-cycle diesel engines / |
2 |
| Y 3.N 21/5:6/839 | Rise in temperature of the charge in its passage through the inlet valve and port of an air-cooled aircraft engine cylinder / | 2 |
| Y 3.N 21/5:6/840 |
Tensile and Pack Compression Tests for Some Sheeets of Aluminum Alloy, 1025 Carbon Steel, and Chromium-Nickel Steel, Feb. 1940. Tensile and pack compressive tests of some sheets of aluminum alloy, 1025 carbon steel, and chromium-nickel steel / |
3 |
| Y 3.N 21/5:6/841 |
The photoviscous properties of fluids / The Photoviscous properties of fluids / |
2 |
| Y 3.N 21/5:6/842 |
Tidewater and weather-exposure tests on metals used in aircraft. Tidewater and weather-exposure tests on metals used in aircraft - II / |
2 |
| Y 3.N 21/5:6/843 |
A summary of results of various investigations of the mechanical properties of aluminum alloys at low temperatures / A Summary of Results of Various Investigations of the Mechanical Properties of Aluminum Alloys at Low Temperatures, May 1942. A Summary of results of various investigations of the mechanical properties of aluminum alloys at low temperatures / |
3 |
| Y 3.N 21/5:6/844 | Investigation of the forces acting on gliders in automobile-, pulley-, winch-, and airplane-towed flight / | 2 |
| Y 3.N 21/5:6/845 | Ground effect on downwash angles and wake location / | 2 |
| Y 3.N 21/5:6/846 | Bending of rectangular plates with large deflections / | 2 |
| Y 3.N 21/5:6/847 | Square plate with clamped edges under normal pressure producing large deflections / | 2 |
| Y 3.N 21/5:6/848 |
Normal -pressure tests of circular plates with clamped edges / Normal-pressure tests of circular plates with clamped edges / |
2 |
| Y 3.N 21/5:6/849 | Normal-pressure tests of rectangular plates / | 2 |
| Y 3.N 21/5:6/850 | A preliminary investigation of the electrical structure of thunderstorms / | 2 |
| Y 3.N 21/5:6/851 | Strength tests of thin-walled elliptic duralumin cylinders in pure bending and in combined pure bending and torsion / | 2 |
