Work

Fluid–structure interaction of panel under swept shock wave/boundary layer interaction

Year: 2024

Type: article

Source: Physics of Fluids

DOI: 10.1063/5.0243593

Authors: Kun Ye, Shubao Chen, Guoliang Li, Pengze Xie, Feng Qu, Zhengyin Ye

Institutions: Northwestern Polytechnical University, Aviation Industry Corporation of China (China), AviChina Industry & Technology (China)

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: G2121417062, G3397435878, G5686462187, G6109458412, G7171238794, G7824822810

OpenAlex ID: W4405611680

FWCI: 1.406

Cites: 40

Cited by: 7

Related to: 10