| タイトル | X-29A for NTF wind-tunnel/flight correlations |
| 著者（英） | Daforno, G. |
| 著者所属（英） | Grumman Aerospace Corp. |
| 発行日 | 1982-06-01 |
| 言語 | eng |
| 内容記述 | Considerations and recommendations for correlation are given. Basic tunnel calibration prior to research and development tests is suggested. Areas of concentration include: wing cruise drag and drag rise, wing separation and stall, afterbody and base drag, propulsion effects, vortex flows, cavity flows, and excrescences. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 82N25210 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/413903 |
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