| タイトル | Evaluation of advanced lift concepts and fuel conservative short-haul aircraft, volume 1 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750012219 |
| 著者（英） | Meyer, R. T.; Patterson, R. W.; Tibbetts, J. G.; Bowden, M. K.; Renshaw, J. H.; Bennett, J. A.; Randall, C. C.; Ferrill, R. S.; Narucki, C. W.; Smith, P. R. |
| 著者所属（英） | Lockheed Aircraft Corp. |
| 発行日 | 1974-06-01 |
| 言語 | eng |
| 内容記述 | The performance and economics of a twin-engine augmentor wing airplane were evaluated in two phases. Design aspects of the over-the-wing/internally blown flap hybrid, augmentor wing, and mechanical flap aircraft were investigated for 910 m. field length with parametric extension to other field lengths. Fuel savings achievable by application of advanced lift concepts to short-haul aircraft were evaluated and the effect of different field lengths, cruise requirements, and noise levels on fuel consumption and airplane economics at higher fuel prices were determined. Conclusions and recommendations are presented. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 75N20291
NASA-CR-137525 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/190574 |
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