Research Paper: LSTM-Based Prediction Method for Supercritical Wing Flutter Boundary
Wang Zihao1 ,Li Gun1 Liu Dawei2 Chen Dehua1, 2 , Zhang Shujun1 1.University of Electronic Science and Technology of China, School of Aerospace Engineering, Chengdu 611731 2.China Aerodynamics Research and Development Center, High-Speed Aerodynamics Institute, Mianyang 621000 doi: 10.7638/kqdlxxb-2023.0146 Abstract The flutter of supercritical wings greatly impacts the safety and stability of transport aircraft. Accurately … Read more
