Boundary layer transition and linear modal instabilities of hypersonic flow over a lifting body
Work
Year: 2022
Type: article
Abstract: Boundary layer transition over a lifting body of 1.6 m length at $2^\circ$ angle of attack has been simulated at Mach 6 and a unit Reynolds number $1.0 \times 10^7$ m $^{-1}$ . The model geometry is t... more
Source: Journal of Fluid Mechanics
Institutions China Aerodynamics Research and Development Center, State Key Laboratory of Aerodynamics
Cites: 58
Cited by: 29
Related to: 10
FWCI: 5.325
Citation percentile (by year/subfield): 99.99
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: bronze
Grant ID 92052301