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Effect of Shock Wave Interference on Aeroelasticity of Hypersonic Airfoils

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Year: 2026
Type: article
Source: AIAA Journal
DOI: 10.2514/1.j065878
Authors: Ye Ma, Kun Ye, Yansong Wang, Feng Qu, Zhengyin Ye
Institution: Northwestern Polytechnical University
Language: English

Topic: Aeroelasticity and Vibration Control
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences

Open Access status: closed

Funders: National Natural Science Foundation of China, Higher Education Discipline Innovation Project, Fundamental Research Funds for the Central Universities
Awards: G5686462187, G6109458412, G7057123751, G7171238794, G7824822810
OpenAlex ID: W7140134131
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Cites: 50
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