| タイトル | Inlet design for high-speed propfans |
| 著者（英） | Little, B. H., Jr.; Hinson, B. L. |
| 著者所属（英） | Lockheed-Georgia Co. |
| 発行日 | 1982-10-01 |
| 言語 | eng |
| 内容記述 | A two-part study was performed to design inlets for high-speed propfan installation. The first part was a parametric study to select promising inlet concepts. A wide range of inlet geometries was examined and evaluated - primarily on the basis of cruise thrust and fuel burn performance. Two inlet concepts were than chosen for more detailed design studies - one apropriate to offset engine/gearbox arrangements and the other to in-line arrangements. In the second part of this study, inlet design points were chosen to optimize the net installed thrust, and detailed design of the two inlet configurations was performed. An analytical methodology was developed to account for propfan slipstream effects, transonic flow efects, and three-dimensional geometry effects. Using this methodology, low drag cowls were designed for the two inlets. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 83A37957
SAE PAPER 821359 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/403550 |
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