摘要
本文用数值方法计算了不同高度滑移边界条件对钝体绕流流场特性的影响。采用化学非平衡粘性激波层控制方程,边界条件含壁面滑移、激波滑移和无滑移条件。计算结果表明,考虑滑移条件后,激波层较厚,激波处的电子数密度为一有限值。文中给出了计算结果,并与其它文献的结果作了比较。
The numerical method is used for calculating the effects of slip boundaryconditions on the viscous flows over blunt bodies at different altitude.Thenonequilibrium viscous shock-layer equations are used as the governingequations,the boundary conditions include shock-slip,wall-slip and no slipconditions.The numerical results show that the shock stand-off distance is thickeras slip boundary conditions are considered,and the value of electron numberdensity behind the bow shock is not zero.The numerical results are pesentedand compared with those from other methods.
出处
《国防科技大学学报》
EI
CAS
CSCD
北大核心
1990年第2期36-43,共8页
Journal of National University of Defense Technology
基金
国家自然科学基金
关键词
高超音速流
粘性流
化学非平衡流
hypersonic flow
viscous flow
blunt body
chemical reacting flow
numerical calculation