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METHOD FOR NUMERICAL MODELING OF UNSTEADY SEPARATED FLOW AROUND AIRFOILS MOVING CLOSE TO FLAT SCREEN

In this article an attempt is made to explain the nature of differences in measurements of forces and moments, which influence an aircraft at take-off and landing when testing on different types of stands. An algorithm for numerical simulation of unsteady separated flow around airfoil is given. The...

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Библиографические подробности
Главные авторы: T. V. Pogrebnaya, S. D. Shipilov
Формат: Artigo
Язык:Russo
Опубликовано: Moscow State Technical University of Civil Aviation 2017-05-01
Серии:Naučnyj Vestnik MGTU GA
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Online-ссылка:https://avia.mstuca.ru/jour/article/view/1056
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