| タイトル | Use of Internal Coolant as a Means of Permitting Increase in Engine Take-Off Power |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930093158 |
| 著者（英） | Rothrock, Addison M |
| 著者所属（英） | National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. |
| 発行日 | 1944-01-01 |
| 言語 | eng |
| 内容記述 | Engine tests, together with estimates made at Langley Memorial Aeronautical Laboratory, indicate that a 25-percent increase in take-off power can be obtained with present-day aircraft engines without increasing either the knock limit of the fuel or the external cooling requirements of the engine. This increase in power with present fuels and present external cooling is made possible through the use of an internal coolant inducted through the inlet manifold. Estimates on aircraft indicate that this 25-percent increase in power will permit an approximate usable increase of 8.5 percent in the take-off load of existing military airplanes. This increase in load is equivalent to an increase in the weight of gasoline normally carried of between 30 and 65 percent. |
| NASA分類 | Aircraft Propulsion and Power |
| レポートNO | 93R22448
NACA-WR-E-117
NACA-RB-4A25 |
| 権利 | No Copyright |
