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Modeling the Flow around a Delta Wing Partially Made of a Permeable Materialстатья
- Авторы: Lutsky A.E., Severin A.V.
- Журнал: Fluid Dynamics
- Том: 59
- Номер: 4
- Год издания: 2024
- Издательство: Maik Nauka/Interperiodica Publishing
- Местоположение издательства: Russian Federation
- Первая страница: 1
- Последняя страница: 12
- Аннотация: Mathematical modeling of a supersonic gas flow around a delta wingat M=2 has been carried out. A wing made of a conventional solid material was compared with a wing whose leading edge was made of a porous material with a porosity coefficient of 0.6. The influenceof a permeable edge on the flow structure and thermal regime is studied.
- Добавил в систему: Луцкий Александр Евгеньевич