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  1. Structure Analysis and Aeroelastic Optimization Method for Composite Wing-box Structure with Curved Fiber
  2. Lateral ground vibration tests for spacecraft
  3. Robust Aeroelastic Design Optimization of Hypersonic Vehicle with Uncertainties in Aerodynamic Loads, Heat Flux, and Structure
  4. A High Efficiency Aeroelastic Analysis Method based on Rigid External Aerodynamic Force and Elastic Correction by High-Order Panel Method