Call Number (LC) | Title | Results |
---|---|---|
Y 3.N 21/5:6/84 | New data on the laws of fluid resistance / | 1 |
Y 3.N 21/5:6/85 | Air Force and three moments for F-5-L seaplane / | 1 |
Y 3.N 21/5:6/86 | Surface area coefficients for airship envelopes / | 1 |
Y 3.N 21/5:6/87 | Hydrostatic test of an airship model / | 1 |
Y 3.N 21/5:6/88 | Test of oil scraper piston ring and piston fitted with oil drain holes / | 1 |
Y 3.N 21/5:6/89 | The choice of the speed of an airship / | 1 |
Y 3.N 21/5:6/90 | Sylphon diaphragms : a method for predicting their performance for purposes of instrument design / | 1 |
Y 3.N 21/5:6/91 | Notes on propeller design. | 1 |
Y 3.N 21/5:6/92 | Full scale determination of the lift and drag of a seaplane / | 1 |
Y 3.N 21/5:6/93 | The background of detonation / | 1 |
Y 3.N 21/5:6/94 | Notes on propeller design. | 1 |
Y 3.N 21/5:6/95 | Notes on propeller design. | 1 |
Y 3.N 21/5:6/96 | Notes on propeller design. | 1 |
Y 3.N 21/5:6/97 | N.A.C.A. control position recorder / | 1 |
Y 3.N 21/5:6/98 | Notes on the design of latticed columns subject to lateral loads / | 1 |
Y 3.N 21/5:6/99 | Notes on the standard atmosphere / | 1 |
Y 3.N 21/5:6/100 |
Theory of the slotted wing / Theory of the slotted wing / |
2 |
Y 3.N 21/5:6/101 | Comparing maximum pressures in internal combustion engines / | 1 |
Y 3.N 21/5:6/102 | Skin frictional resistance of plane surfaces in air : abstract of recent German tests, with notes / | 1 |
Y 3.N 21/5:6/103 | Simple formula for estimating airplane ceilings / | 1 |