TY  - CONF

T1  - A new numerical method for solving supersonic separated flows over a compression corner by introducing an interactive boundary condition

JO  - Proceedings of the Third National Conference on Computational Fluid Dynamics

PY  - 1985/09/01

AU  - Qin N

AU  - Cao CP

ED  - 

Y2  - 2024/12/27

ER  -