All Stories

  1. Aircraft Community Noise Propagation Using Gaussian Beam Tracing with Moving Sources
  2. Improved Turboelectric System Modeling for Conceptual Design of HEPS Aircraft
  3. Aero-Propulsive Coupling Simulation of a Wing with Distributed Ducted-Fans
  4. A Framework for Deriving Top-Level Requirements in UAM Ecosystem with System Performance Considerations
  5. Development of Liquid-Cooled Battery System Sizing Method for eVTOL Aircraft
  6. Preliminary Propeller Anti-Icing Design for Expanding the Icing Operational Envelope of HALE UAVs
  7. A Simulation Framework for Performance and Safety Evaluation of a Hovering Rotor in Icing Conditions
  8. A System-Level Design Framework for Collaborative Unmanned Vehicles – Part I. Design Process
  9. Trajectory Optimization of Dual Mode Scramjet Engine Vehicle Using a Refined Quasi One-Dimensional Combustion Model
  10. Development of Air-Cooled Battery Sizing Method for eVTOL Aircraft
  11. Numerical Analysis of the Effect of Propeller Wake on Wing Icing Characteristics
  12. Understanding the Impact of Ice on Propellers and High-Altitude UAV Flight Performance
  13. Leveraging Deep Neural Networks for Efficient Prediction of Aerodynamic Performance Tables
  14. Novel Electric Propulsion System Analysis Method for Electric Vertical Takeoff and Landing Aircraft Conceptual Design
  15. Landing Trajectory Analysis of eVTOL Aircraft for Urban Air Mobility Considering Vortex Ring State
  16. Physically interpretable airfoil parameterization using variational autoencoder-based generative modeling
  17. Mesh Generation for Flow Analysis by using Deep Reinforcement Learning
  18. Physics-aware reduced-order modeling of transonic flow via β-variational autoencoder
  19. Assessment of High-Order Schemes for Vortex-Dominated Flowfield Using Truncation Error Analysis
  20. Technology Portfolio Assessment with Uncertainty Consideration for Advanced Air Mobility
  21. Development of Fuel Cell/Battery Hybrid System Sizing Methodology for eVTOL Aircraft
  22. Prediction of Rotor Aerodynamic Force and Noise using Reduced Order Model
  23. Novel optimization method for the aeroelastic design of composite rotor blades
  24. Local non‐intrusive reduced order modeling based on soft clustering and classification algorithm
  25. Generic Design Methodology for Vertical Takeoff and Landing Aircraft with Hybrid-Electric Propulsion
  26. New Roughness-Induced Transition Model for Simulating Ice Accretion on Airfoils
  27. Aerodynamic Efficiency Optimization of the 1st Stage of Transonic High Pressure Turbine through Lean and Sweep Angles
  28. Variable-Fidelity Optimization of Film-Cooling Hole Arrangements Considering Conjugate Heat Transfer
  29. High-to-Low Initial Sample Ratio of Hierarchical Kriging for Film Hole Array Optimization
  30. Procedure for Determining Operation Limits of High-Altitude Long-Endurance Aircraft Under Icing Conditions
  31. Optimum Arrangement of Film Cooling Holes Considering the Manufacturing Tolerance
  32. Ice Accretion on Helicopter Fuselage Considering Rotor-Wake Effects
  33. Variable Fidelity Optimization of Film Cooling Hole Arrangement Considering Internal Cooling Effects
  34. Optimization of Film Cooling Hole Array Considering the Variation of Turbine Inlet Temperature Profiles
  35. Optimization of the Array of Film-Cooling Holes on a High-Pressure Turbine Nozzle
  36. Numerical Prediction of Scientific Balloon Trajectories While Considering Various Uncertainties
  37. Modification of Multiresolution Analysis for Efficient Implicit Temporal Integration
  38. Cost Effective Multi-Resolution Analysis Applied to Implicit Temporal Integration
  39. Efficiency Enhancement of Reduced Order Model using Variable Fidelity Modeling