作者: Xian Liang , Xinliang Li , Dexun Fu , Yanwen Ma
DOI: 10.1016/J.COMPFLUID.2009.09.015
关键词: Boundary layer 、 Mechanics 、 Adiabatic wall 、 Computational fluid dynamics 、 Isothermal process 、 Classical mechanics 、 Mathematics 、 Linear stability 、 Direct numerical simulation 、 Hypersonic speed 、 Mach number 、 General Engineering 、 General Computer Science
摘要: … on the stability of boundary layer for hypersonic flow, mainly considering the effect of wall temperature. The … thickness due to difference wall temperature leads to the change of instability …