| タイトル | Turboprop Cargo Aircraft Systems study, phase 1 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810007526 |
| 著者（英） | Hewell, J. G., Jr.; Muehlbauer, J. C.; Searle, N.; Stone, F. R., Jr.; Randall, C. C.; Lindenbaum, S. P. |
| 著者所属（英） | Lockheed-Georgia Co. |
| 発行日 | 1980-11-01 |
| 言語 | eng |
| 内容記述 | The effects of advanced propellers (propfan) on aircraft direct operating costs, fuel consumption, and noiseprints were determined. A comparison of three aircraft selected from the results with competitive turbofan aircraft shows that advanced turboprop aircraft offer these potential benefits, relative to advanced turbofan aircraft: 21 percent fuel saving, 26 percent higher fuel efficiency, 15 percent lower DOCs, and 25 percent shorter field lengths. Fuel consumption for the turboprop is nearly 40 percent less than for current commercial turbofan aircraft. Aircraft with both types of propulsion satisfy current federal noise regulations. Advanced turboprop aircraft have smaller noiseprints at 90 EPNdB than advanced turbofan aircraft, but large noiseprints at 70 and 80 EPNdB levels, which are usually suggested as quietness goals. Accelerated development of advanced turboprops is strongly recommended to permit early attainment of the potential fuel saving. Several areas of work are identified which may produce quieter turboprop aircraft. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 81N16041
LG80ER0112
NASA-CR-159355 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/170314 |
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