SIMULATION OF AIRCRAFT CONDENSATION TRAILS AND WAKE VORTICES INTERACTION
A technique of calculation of aircraft condensation trails (contrails) and wake vortices interaction is described. The technique is based on a suitable for real-time applications mathematical model of far wake utilizes the method of discrete vortices. The technique is supplemented by account of the...
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| Huvudupphov: | , , , |
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| Materialtyp: | Artigo |
| Språk: | Russo |
| Utgiven: |
Moscow State Technical University of Civil Aviation
2016-11-01
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| Serie: | Научный вестник МГТУ ГА |
| Ämnen: | |
| Länkar: | https://avia.mstuca.ru/jour/article/view/118 |
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