2 papers
physics.flu-dyn2026
A Three-Dimensional Two-Temperature Gas-Kinetic Scheme with Generalized Kinetic Boundary Condition for Hypersonic SBLI
Xingjian Gao, Hualin Liu, Fengxiang Zhao +1
Accurate prediction of aerothermal loads in hypersonic flows is critical yet challenging due to the coupling of Shock-Wave/Boundary-Layer Interactions (SBLI) and thermal non-equili…
physics.flu-dyn2026
A two-temperature gas-kinetic scheme for hypersonic nonequilibrium flow computations
Xingjian Gao, Xing Ji, Hualin Liu +1
Accurate aerodynamic and aerothermodynamic predictions are crucial for numerous hypersonic applications. This paper proposes a gas-kinetic scheme (GKS) coupled with a two-temperatu…