Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers

作者: Xiaolin Zhong , Xiaowen Wang

DOI: 10.1146/ANNUREV-FLUID-120710-101208

关键词: Computational fluid dynamicsDragDirect numerical simulationBoundary (topology)Aerospace engineeringLaminar-turbulent transitionHypersonic speedAerodynamic heatingComputer scienceInstability

摘要: The prediction of the laminar-turbulent transition of boundary layers is critically important to the development of hypersonic vehicles because the transition has a first-order impact on …

参考文章(168)
L. Kleiser, N. D. Sandham, N. A. Adams, Y. Guo, Numerical Simulation of Supersonic Boundary Layer Transition adle. ,(1994)
Mark V. Morkovin, On the Many Faces of Transition Springer, Boston, MA. pp. 1- 31 ,(1969) , 10.1007/978-1-4899-5579-1_1
A. D. Kosinov, N. V. Semionov, S. G. Shevel’kov, O. I. Zinin, Experiments on the Nonlinear Instability of Supersonic Boundary Layers Springer, Berlin, Heidelberg. pp. 196- 205 ,(1994) , 10.1007/978-3-642-85084-4_17