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作者:Ryszard Makarowski , Andrzej Piotrowski
来源:[J].Medycyna Pracy(IF 0.391), 2017, Vol.68 (5), pp.639-651DOAJ
摘要:... Material and Methods: We examined 97 male pilots of passenger planes, who had flew ATRs, Boeings, Airbuses, Embraers, and Saabs. The comparative group was made up of 127 graduates of technical studies (not connected with aviation). In our study, we used the following metho...
作者:Oren E. Nahum , Yuval Hadas , Assaf Kalish
来源:[J].Transportation Research Procedia, 2019, Vol.37, pp.354-361Elsevier
摘要:Abstract(#br)From the beginning of the 20th century, transporting passengers and cargo has changed due to the advancements in aircraft design. In the last decade, there have also been changes in the levels of technology, information sharing, the distribution of flight data kn...
作者:Qingjiang Zhang , Xinmin Wang , Yan Li
来源:[J].Energy Procedia, 2011, Vol.13, pp.848-854Elsevier
摘要:Abstract(#br)On the base of analysising the large-type passenger plane's characteristics, combining with flight quality requirements for manned aircraft, this article convered the flight quality requirements into the regional limits for closed-loop pole assignment,then optimized ...
作者:T Watanabe , K Matsushima , K Nakahashi
来源:[J].Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering(IF 0.4), 2008, Vol.222 (7), pp.1025-1035Sage国际出版集团
摘要:Abstract(#br)In this article, aerodynamic optimization of a near-sonic passenger plane was conducted, starting with a conventional tail configuration. The genetic algorithm (GA) combined with the Euler simulations were used to maximize the lift-to-drag ratio ( L / D ) at Mach 0.9...
作者:Watanabe, T , Matsushima, K , Nakahashi, K
来源:[J].Proceedings of the Institution of Mechanical Engineers(IF 0.4), 2008, Vol.222 (G7), pp.1025-1035ProQuest
摘要:In this article, aerodynamic optimization of a near-sonic passenger plane was conducted, starting with a conventional tail configuration. The genetic algorithm (GA) combined with the Euler simulations were used to maximize the lift-to-drag ratio (L/D) at Mach 0.95. First, the win...
作者:A. Ya. Chervonenkis , S. S. Chernova , T. V. Zykova
来源:[J].Automation and Remote Control(IF 0.192), 2011, Vol.72 (5), pp.1061-1067Springer
摘要:Abstract(#br)We show the results of applying the kernel ridge regression method to the problem of fast computation of aerodynamical characteristics of an airplane. We compare our results with the results found with surrogate models constructed with artificial neural networks.
作者:Rang Shu Xu , Nana Zhang , Ling Niu ...
来源:[J].Applied Mechanics and Materials, 2012, Vol.2025, pp.855-858Trans Tech
摘要:In order to study heat transfer process in APU compartment of passenger plane and to perform structure thermal analysis, temperature field of APU compartment has been calculated by numerical computation. The computation model of flow and heat transfer process in APU compartmen...
作者:顾恒山
来源:[D].上海交通大学  2011CNKI
摘要:飞机的坠撞安全性是指民用飞机应急着陆时机体结构具有的保护乘员生命安全的能力。中国民用航空总局颁布的《运输类飞机适航标准》中规定了飞机应急着陆时的动力要求。因此民用飞机的坠撞安全性成...
被引频次:1下载频次:157
作者:Makarowski Ryszard , Piotrowski Andrzej
来源:[J].Medycyna pracy(IF 0.391), 2017, Vol.68 (5), pp.639-651PubMed
摘要:...We examined 97 male pilots of passenger planes, who had flew ATRs, Boeings, Airbuses, Embraers, and Saabs. The comparative group was made up of 127 graduates of technical studies (not connected with aviation). In our study, we used the following methods: the PTS (Pavlovian Te...

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