| Call Number (LC) | Title | Results |
|---|---|---|
| Y 3.N 21/5:6/347 |
The pressure distribution over a Douglas wing tip on a biplane in flight / The Pressure distribution over a Douglas wing tip on a biplane in flight / |
2 |
| Y 3.N 21/5:6/348 | Alterations and tests of the "Farnboro" engine indicator / | 2 |
| Y 3.N 21/5:6/349 |
An investigation of airplane landing speeds / An Investigation of airplane landing speeds / c Kenneth F. Ridley. |
2 |
| Y 3.N 21/5:6/350 | Methods for the identification of aircraft tubing of plain carbon steel and chromium-molybdenum steel / | 2 |
| Y 3.N 21/5:6/351 |
An accurate method of measuring the moments of inertia of airplanes / An Accurate method of measuring the moments of inertia of airplanes / |
2 |
| Y 3.N 21/5:6/352 | Effect of orifice length-diameter ratio on spray characteristics / | 2 |
| Y 3.N 21/5:6/353 | Analytical determination of the load on a trailing edge flap / | 2 |
| Y 3.N 21/5:6/354 |
An investigation of the phenomenon of separation in the air flow around simple quadric cylinders / An Investigation of the phenomenon of separation in the air flow around simple quadric cylinders / |
2 |
| Y 3.N 21/5:6/355 | Effect of the angular position of the section of a ring cowling on the high speed of an XF7C-1 airplane / | 2 |
| Y 3.N 21/5:6/356 | Some characteristics of fuel sprays from open nozzles / | 2 |
| Y 3.N 21/5:6/357 | Bending tests of metal monocoque fuselage construction / | 2 |
| Y 3.N 21/5:6/358 | Experiments with a model water tunnel / | 2 |
| Y 3.N 21/5:6/359 |
A balanced diaphragm type of maximum cylinder pressure indicator / A Balanced diaphragm type of maximum cylinder pressure indicator / |
2 |
| Y 3.N 21/5:6/360 |
The pressure distribution over a square wing tip on a biplane in flight / The Pressure distribution over a square wing tip on a biplane in flight / |
2 |
| Y 3.N 21/5:6/361 |
The effect of small variations in profile of airfoils / The Effect of small variations in profile of airfoils / |
2 |
| Y 3.N 21/5:6/362 | Lift and drag characteristics of a cabin monoplane determined in flight / | 2 |
| Y 3.N 21/5:6/363 |
The behavior of conventional airplanes in situations thought to lead to most crashes / The Behavior of conventional airplanes in situations thought to lead to most crashes / |
2 |
| Y 3.N 21/5:6/364 | Tests in the Variable Density Wind Tunnel to investigate the effects of scale and turbulence on airfoil characteristics / | 2 |
| Y 3.N 21/5:6/365 | Interference effects and drag of struts on a monoplane wing / | 2 |
| Y 3.N 21/5:6/366 | Torsion in box wings / | 2 |
