High-temperature effects in hypersonic flows
نویسندگان
چکیده
منابع مشابه
A high-order numerical method to study hypersonic boundary-layer instability including high-temperature gas effects
Prediction of laminar-turbulent transition is a key factor in the design of the heat shield of vehicles (re-)entering a planetary atmosphere. To investigate the transition by means of numerical simulation, accurate and efficient computational methods are necessary. Here, the compressible Navier–Stokes equations are solved for a gas where properties such as specific heat, thermal conductivity, v...
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ژورنال
عنوان ژورنال: Sadhana
سال: 1995
ISSN: 0256-2499,0973-7677
DOI: 10.1007/bf02744410