中南大学赵雅甜

当前位置: 中文主页 >> 论文成果

Active control method for restart performances of hypersonic inlets based on energy addition

发布时间：2020-09-15

点击次数：

影响因子：2.829

发表刊物：Aerospace Science and Technology

论文类型：期刊论文

文献类型：J

是否译文：否

收录刊物：SCI

上一条： Uncertainty and sensitivity analysis of flow parameters for transition models on hypersonic flows

下一条： Numerical study of the cone angle effects on transition and convection heat transfer for hy-personic inflatable aerodynamic decelerator aeroshell