Work

Nonlinear Aeroelastic Behavior of a Panel Subjected to Oscillating Shock Waves

Year: 2026

Type: article

Source: AIAA Journal

DOI: 10.2514/1.j066113

Authors: Shentai Wu, Kun Ye, Bin Wu, 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

Awards: G5686462187, G6109458412, G7171238794, G7824822810

OpenAlex ID: W7162021759

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Cites: 40

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