APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS

APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS

Applicability of the open source package OpenFOAM for numerical modeling different separated flows have been considered in the cases studies of the influence of vortices and their interaction with lifting surfaces, features of the flow field of rapidly rotating aerial vehicles at presence of separat...

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Bibliographic Details
Main Authors: V. T. Kalugin, A. G. Golubev, A. S. Epikhin, A. A. Michkin
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2017-01-01
Series:Научный вестник МГТУ ГА
Subjects:
пакет openfoam
отрывное течение
обтекание тел с излом образующей
быстровращающиеся летательные аппараты
сверхзвуковое отрывное обтекание
Online Access:https://avia.mstuca.ru/jour/article/view/961

Internet

https://avia.mstuca.ru/jour/article/view/961

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