Study of a supersonic reacting wall jet with a variable turbulent Prandtl and Schmidt number approach

Aerospace Science and Technology - Tập 106 - Trang 106070 - 2020
J.J.O.E. Hoste1, S. Fechter1, S. Karl1, K. Hannemann1
1Institute of Aerodynamics and Flow Technology, German Aerospace Center (DLR), Bunsenstraße 10, 37073 Göttingen, Germany

Tài liệu tham khảo

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