All Stories

  1. Novel Electric Propulsion System Analysis Method for Electric Vertical Takeoff and Landing Aircraft Conceptual Design
  2. Landing Trajectory Analysis of eVTOL Aircraft for Urban Air Mobility Considering Vortex Ring State
  3. Physically interpretable airfoil parameterization using variational autoencoder-based generative modeling
  4. Mesh Generation for Flow Analysis by using Deep Reinforcement Learning
  5. Physics-aware reduced-order modeling of transonic flow via β-variational autoencoder
  6. Assessment of High-Order Schemes for Vortex-Dominated Flowfield Using Truncation Error Analysis
  7. Technology Portfolio Assessment with Uncertainty Consideration for Advanced Air Mobility
  8. Development of Fuel Cell/Battery Hybrid System Sizing Methodology for eVTOL Aircraft
  9. Prediction of Rotor Aerodynamic Force and Noise using Reduced Order Model
  10. Novel optimization method for the aeroelastic design of composite rotor blades
  11. Local non‐intrusive reduced order modeling based on soft clustering and classification algorithm
  12. Generic Design Methodology for Vertical Takeoff and Landing Aircraft with Hybrid-Electric Propulsion
  13. New Roughness-Induced Transition Model for Simulating Ice Accretion on Airfoils
  14. Aerodynamic Efficiency Optimization of the 1st Stage of Transonic High Pressure Turbine through Lean and Sweep Angles
  15. Variable-Fidelity Optimization of Film-Cooling Hole Arrangements Considering Conjugate Heat Transfer
  16. High-to-Low Initial Sample Ratio of Hierarchical Kriging for Film Hole Array Optimization
  17. Procedure for Determining Operation Limits of High-Altitude Long-Endurance Aircraft Under Icing Conditions
  18. Optimum Arrangement of Film Cooling Holes Considering the Manufacturing Tolerance
  19. Ice Accretion on Helicopter Fuselage Considering Rotor-Wake Effects
  20. Variable Fidelity Optimization of Film Cooling Hole Arrangement Considering Internal Cooling Effects
  21. Optimization of Film Cooling Hole Array Considering the Variation of Turbine Inlet Temperature Profiles
  22. Optimization of the Array of Film-Cooling Holes on a High-Pressure Turbine Nozzle
  23. Numerical Prediction of Scientific Balloon Trajectories While Considering Various Uncertainties
  24. Modification of Multiresolution Analysis for Efficient Implicit Temporal Integration
  25. Cost Effective Multi-Resolution Analysis Applied to Implicit Temporal Integration
  26. Efficiency Enhancement of Reduced Order Model using Variable Fidelity Modeling