| タイトル | Current and future technology in radial and axial gas turbines |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830024540 |
| 著者（英） | Rohlik, H. E. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1983-08-27 |
| 言語 | eng |
| 内容記述 | Design approaches and flow analysis techniques currently employed by aircraft engine manufacturers are assessed. Studies were performed to define the characteristics of aircraft and engines for civil missions of the 1990's and beyond. These studies, coupled with experience in recent years, identified the critical technologies needed to meet long range goals in fuel economy and other operating costs. Study results, recent and current research and development programs, and an estimate of future design and analytic capabilities are discussed. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 83N32811
NASA-TM-83414
E-1702
NAS 1.15:83414 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/161788 |
