Computer modeling of exhaust jet flux interaction with deflecting shield
Abstract
Method of exhaust jet flux interaction with deflecting shield computer modeling is proposed in this article. The article is devoted to concrete ecological task - to decrease the noise influence on ground maintenance stuff and passengers in the airports. The method is based on the Reynolds equation system solution obtained with the help of control volume method. Calculation results give an opportunity to choose main deflecting shield parameters according to concrete airport conditions.
References
1. Абрамович Г.Н. Теория турбулентных струй. - М.: Физматгиз, 1960.
2. Абрамович Г.Н., Крашенинников С.Ю., Секундов А.Н., Смирнова И.П. Турбулентное смешение газовых струй. - М.: Наука, 1974.
Review
For citations:
Kartishev O.A. Computer modeling of exhaust jet flux interaction with deflecting shield. Civil Aviation High Technologies. 2014;(208):54-59. (In Russ.)
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