| タイトル | Integrated gas turbine engine-nacelle |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790005925 |
| 著者（英） | Stotler, C. L., Jr.; Adamson, A. P.; Sargisson, D. F. |
| 著者所属（英） | NASA Lewis Research Center|General Electric Co. |
| 発行日 | 1979-01-02 |
| 言語 | eng |
| 内容記述 | A nacelle for use with a gas turbine engine is provided with an integral webbed structure resembling a spoked wheel for rigidly interconnecting the nacelle and engine. The nacelle is entirely supported in its spacial relationship with the engine by means of the webbed structure. The inner surface of the nacelle defines the outer limits of the engine motive fluid flow annulus, while the outer surface of the nacelle defines a streamlined envelope for the engine. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 79N14096 |
| 権利 | No Copyright |
