| タイトル | Design and evaluation of an integrated Quiet, Clean General Aviation Turbofan (QCGAT) engine and aircraft propulsion system |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810023604 |
| 著者（英） | Wilson, C.; German, J.; Fogel, P. |
| 著者所属（英） | Avco Lycoming Div. |
| 発行日 | 1980-04-01 |
| 言語 | eng |
| 内容記述 | The design was based on the LTS-101 engine family for the core engine. A high bypass fan design (BPR=9.4) was incorporated to provide reduced fuel consumption for the design mission. All acoustic and pollutant emissions goals were achieved. A discussion of the preliminary design of a business jet suitable for the developed propulsion system is included. It is concluded that large engine technology can be successfully applied to small turbofans, and noise or pollutant levels need not be constraints for the design of future small general aviation turbofan engines. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 81N32147
LYC-80-27
NASA-CR-165185 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/168042 |
