| 書目名稱 | Vortex wakes of Aircrafts |
| 編輯 | A.S. Ginevsky,A. I. Zhelannikov |
| 視頻video | http://file.papertrans.cn/986/985031/985031.mp4 |
| 概述 | Combines method of discrete vortices with Integral methods.Efficient approach helps to drastically reduce calculation times.Includes supplementary material: |
| 叢書名稱 | Foundations of Engineering Mechanics |
| 圖書封面 |  |
| 描述 | Investigation of vortex wakes behind various aircraft, especially behind wide bodied and heavy cargo ones, is of both scientific and practical in terest. The vortex wakes shed from the wing’s trailing edge are long lived and attenuate only atdistances of10–12kmbehindthe wake generating aircraft. The encounter of other aircraft with the vortex wake of a heavy aircraft is open to catastrophic hazards. For example, air refueling is adangerous operationpartly due to thepossibility of the receiver aircraft’s encountering the trailing wake of the tanker aircraft. It is very important to know the behavior of vortex wakes of aircraft during theirtakeoff andlanding operations whenthe wakes canpropagate over the airport’s ground surface and be a serious hazard to other depart ing or arriving aircraft. This knowledge can help in enhancing safety of aircraft’s movements in the terminal areas of congested airports where the threat of vortex encounters limits passenger throughput. Theoreticalinvestigations of aircraft vortex wakes arebeingintensively performedinthe major aviationnations.Usedforthispurpose are various methods for mathematical modeling of turbulent flows: direct numerical simulati |
| 出版日期 | Book 2009 |
| 關鍵詞 | Atmospheric Turbulence; Descrete Vortices; Integral Method; Landing; Take-off; Turbulent Boundary Layer; m |
| 版次 | 1 |
| doi | https://doi.org/10.1007/978-3-642-01760-5 |
| isbn_softcover | 978-3-642-24246-5 |
| isbn_ebook | 978-3-642-01760-5Series ISSN 1612-1384 Series E-ISSN 1860-6237 |
| issn_series | 1612-1384 |
| copyright | Springer-Verlag Berlin Heidelberg 2009 |
|Archiver|手機版|小黑屋|
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