Numerical and experimental research on progressive damage of composite stiffened panels during post-buckling analysis
Year: 2024
Type: conference-paper
DOI: 10.1117/12.3046936
Authors: Baocai Pang, Zhao Zhang, Fei Yuan
Institution: Aircraft Strength Research Institute (China)
Language: English
Subfield: Mechanics of Materials
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4402912427
