作者: Xiaolin Zhong , Xiaowen Wang
DOI: 10.1146/ANNUREV-FLUID-120710-101208
关键词: Computational fluid dynamics 、 Drag 、 Direct numerical simulation 、 Boundary (topology) 、 Aerospace engineering 、 Laminar-turbulent transition 、 Hypersonic speed 、 Aerodynamic heating 、 Computer science 、 Instability
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 …