Analysis Method of Flight Test Results of Large Aspect Ratio wing Maneuvering Load Alleviation and CFD Simulation Verification
Year: 2024
Type: conference-paper
Authors: Fan Jielin, Mao Kun, Wu Dawei, Si Jiangtao, Pan Lijun, Liu Yang
Institution: Commercial Aircraft Corporation of China (China)
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4411409724
