| タイトル | Analysis of regenerated single-shaft ceramic gas-turbine engines and resulting fuel economy in a compact car |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770022663 |
| 著者（英） | Klann, J. L.; Tew, R. C., Jr. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1977-08-01 |
| 言語 | eng |
| 内容記述 | Ranges in design and off-design operating conditions of an advanced gas turbine and their effects on fuel economy were analyzed. The assumed engine incorporated a single stage radial flow turbine and compressor with fixed geometry. Fuel economies were calculated over the composite driving cycle with gasoline as the fuel. At a constant turbine-inlet temperature, with a regenerator sized for a full power effectiveness the best fuel economies ranged from 11.1 to 10.2 km/liter (26.2 to 22.5 mpg) for full power turbine tip speeds of 770 to 488m/sec (2530 to 1600ft/sec), respectively. |
| NASA分類 | ENERGY PRODUCTION AND CONVERSION |
| レポートNO | 77N29607
NASA-TM-X-3531
E-9103 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/181522 |
