| タイトル | Computational thermo-fluid dynamics contributions to advanced gas turbine engine design |
| 著者（英） | Graham, R. W.; Adamczyk, J. J.; Rohlik, H. E. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1985-01-01 |
| 言語 | eng |
| 内容記述 | The design practices for the gas turbine are traced throughout history with particular emphasis on the calculational or analytical methods. Three principal components of the gas turbine engine will be considered: namely, the compressor, the combustor and the turbine. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 85A19509
AIAA PAPER 85-0083 |
| 権利 | Copyright |
