Simulations of an Unsteady Three-dimensional Hypersonic Double-cone Flow at Mach 10.4

Presentation information

Oral presentation

Incompressible/compressible/hypersonic flow

Thu. Jul 18, 2024 2:00 PM - 4:00 PM Room D

Chair:Ayato Takii

2:00 PM - 2:30 PM

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

Keywords:boundary layer separation, hypersonic flow, high-speed flow

Abstract password authentication.
Password is required to view the abstract. Please enter a password to authenticate.