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Design and analysis of a fuel-efficient single-engine, turboprop-powered, business airplane
| 题名： | Design and analysis of a fuel-efficient single-engine, turboprop-powered, business airplane |
| 作者： | Martin, G. L.; Everest, D. E., Jr.; Lovell, W. A.; Price, J. E.; Walkley, K. B.; Washburn, G. F. |
| 关键词： | turbo；sines；analysis；design；single；engine；power；cruise；fici；lane |
| 摘要： | The speed, range, payload, and fuel efficiency of a general aviation airplane powered by one turboprop engine was determined and compared to a twin engine turboprop aircraft. An airplane configuration was developed which can carry six people for a noreserve range of 2,408 km at a cruise speed above 154 m/s, and a cruise altitude of about 9,144 m. The cruise speed is comparable to that of the fastest of the current twin turboprop powered airplanes. It is found that the airplane has a cruise specific range greater than all twin turboprop engine airplanes flying in its speed range and most twin piston engine airplanes flying at considerably slower cruise airspeeds. |
| 报告类型： | 科技报告 |
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