| Call Number (LC) | Title | Results |
|---|---|---|
| Y 3.N 21/5:6/499 | Effect of retractable-spoiler location on rolling- and yawing-moment coefficents / | 2 |
| Y 3.N 21/5:6/500 | The torsional stiffness of thin duralumin shells subjected to large torques / | 2 |
| Y 3.N 21/5:6/501 | Landing-shock recorder / | 2 |
| Y 3.N 21/5:6/502 | Aerodynamic investigation of a cup anemometer / | 2 |
| Y 3.N 21/5:6/503 | Measurement of altitude in blind flying / | 2 |
| Y 3.N 21/5:6/504 | Complete tank tests of two flying-boat hulls with pointed steps - N.A.C.A. Models 22-A and 35 / | 2 |
| Y 3.N 21/5:6/505 | The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing / | 2 |
| Y 3.N 21/5:6/506 | Experimental verification of Theodorsen's theoretical jet-boundary correction factors / | 2 |
| Y 3.N 21/5:6/507 |
The effects of equal-pressure fixed slots on the characteristics of a Clark Y aerofoil / The effects of equal-pressure fixed slots on the characteristics of a Clark Y airfoil / |
2 |
| Y 3.N 21/5:6/508 | Landing characteristics of an autogiro / | 2 |
| Y 3.N 21/5:6/509 |
Tank tests of flat and V-bottom planing surfaces / Tank tests of flat and v-bottom planing surfaces / |
2 |
| Y 3.N 21/5:6/510 | The calculated effect of trailing-edge flaps on the take-off of flying boats / | 2 |
| Y 3.N 21/5:6/511 | A study of the pitching moments and the stability characteristics of monoplanes / | 2 |
| Y 3.N 21/5:6/512 |
A complete tank test of the hull of the Sikorsky S-40 flying boat - American Clipper Class / A complete tank test on the hull of the Sikorsky S-40 flying boat - American Clipper Class / |
2 |
| Y 3.N 21/5:6/513 | The wave suppressors used in the N.A.C.A. tank / | 2 |
| Y 3.N 21/5:6/514 | Effect of combustion-chamber shape on the performance of a prechamber compression-ignition engine / | 2 |
| Y 3.N 21/5:6/515 | Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model / | 2 |
| Y 3.N 21/5:6/516 | Propeller vibrations and the effect of the centrifugal force / | 1 |
| Y 3.N 21/5:6/517 | The aerodynamic forces and moments on a spinning model of the F4B-2 airplane as measured by the spinning balance / | 1 |
| Y 3.N 21/5:6/518 | Performance tests of a single-cylinder compression-ignition engine with a displacer piston / | 1 |
