Analysis and modelling of unsteady oblique shock trains under asymmetric incoming boundary layers
Year: 2026
Type: article
Source: Journal of Fluid Mechanics
Institution: Nanjing University of Aeronautics and Astronautics
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G205735179, G4508470835
OpenAlex ID: W7154609785
