Investigation of high-speed boundary-layer transition by DNS
نویسندگان
چکیده
منابع مشابه
Investigation of Thermal Nonequilibrium on Hypersonic Boundary-Layer Transition by DNS
High-temperature gas effects are known as the physical processes which result in a deviation of the behavior of the calorically perfect gas in the hypersonicflow regime. These effects may have a significant impact on laminar-turbulent transition of the boundary layer, and thus affect the heat loads of hypersonic vehicles. In the present paper we deal with thermal effects, i.e. rotational and vi...
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ژورنال
عنوان ژورنال: PAMM
سال: 2004
ISSN: 1617-7061,1617-7061
DOI: 10.1002/pamm.200410216