Volume 43 Issue 7
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HUANG Chengtao, WANG Lixin, ZHONG Bowenet al. Quantified effects of high-altitude wind on route performance of large passenger plane[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(7): 1348-1354. doi: 10.13700/j.bh.1001-5965.2016.0542(in Chinese)
Citation: HUANG Chengtao, WANG Lixin, ZHONG Bowenet al. Quantified effects of high-altitude wind on route performance of large passenger plane[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(7): 1348-1354. doi: 10.13700/j.bh.1001-5965.2016.0542(in Chinese)

Quantified effects of high-altitude wind on route performance of large passenger plane

doi: 10.13700/j.bh.1001-5965.2016.0542
Funds:

National High-tech Research and Development Program of China 2014AA110501

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  • Corresponding author: HUANG Chengtao, E-mail: hct113a@aliyun.com
  • Received Date: 22 Jun 2016
  • Accepted Date: 25 Aug 2016
  • Publish Date: 20 Jul 2017
  • High-altitude wind affects the fuel consumption and flight time of large passenger plane route flight. This paper is aimed at proposing a method to calculate the route performance of aircraft in high-altitude wind, and analyzing the effects of high-altitude wind on route performance of large passenger plane. A flight simulation model of aircraft in the wind was established. A pilot modeling method for aircraft route flight was proposed. Based on the "pilot-aircraft" closed-loop digital virtual flight simulation, a method to calculate the route performance of aircraft in high-altitude wind was proposed. The fuel consumption, flight time and flight distance of the example aircraft under the typical route were calculated and analyzed. The study shows that, in the same flight distance, the fuel consumption and flight time of the plane are reduced by the tailwind and increased by the headwind. Due to the effects of high-altitude wind, the fuel consumption and flight time can be big difference in some round-trip route. In some long-distance route, due to the effects of high-altitude wind, in order to meet the maximum takeoff weight limit, the payload should be reduced to load more fuel, so as to reach the terminal airport.

     

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