Incompressible/compressible/hypersonic flow-IV

[11-D-01] Simulations of an Unsteady Three-dimensional Hypersonic Double-cone Flow at Mach 10.4

*Cheng Li¹, Jiaao Hao¹ (1. Department of Aeronautical and Aviation Engineering, The Hong Kong Polytechnic University, Kowloon, Hong Kong)

キーワード：boundary layer separation, hypersonic flow, high-speed flow