Work

Fluid–structure interaction effects on shock-wave/boundary-layer interaction in a supersonic compression-corner flow

Year: 2026

Type: article

Source: Aerospace Science and Technology

DOI: 10.1016/j.ast.2026.113529

Authors: Hong Wei, Kun Ye, Yunhao Li, Zhengyin Ye

Institution: Northwestern Polytechnical University

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funders: National Natural Science Foundation of China, Higher Education Discipline Innovation Project

Awards: G5686462187, G6109458412, G7171238794, G7824822810

OpenAlex ID: W7202381642

FWCI:

Cites: 38

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