All Stories

  1. Air Cargo Operations Research: Current Limitations and Future Directions
  2. Comparing the Momentum Contribution Field for RANS and DDES-Based Primal Solutions
  3. Trim Strategies and Dynamic Cross-Coupling During Aerial Refueling
  4. A Sensitivity-Driven Approach to Automotive Aerodynamic Design
  5. Neural-Network-Based Soaring Flight in Randomized Environments
  6. Application of Leading-Edge Tubercles on Rotor Blades
  7. Effect of Leading-Edge Tubercles on Vertical Axis Wind Turbine Performance
  8. Improving Dynamic Stall Effects Using Leading Edge Tubercles
  9. Effect of Leading Edge Tubercles on Tilt-Wing Transition
  10. Optimization of Leading Edge Tubercles Applied to Helicopter Rotor Blades
  11. Effect of Various Cambered Airfoil Profiles to Wings with Leading Edge Tubercles in Transonic Flow
  12. Application of Leading-Edge Tubercles to Enhance Propeller Performance
  13. The Effect of Manufacturing Variation on Aerodynamic Performance and Flight Safety
  14. Effect of Leading-Edge Tubercles on Rotor Blades
  15. Novel Parameters for the Performance Evaluations of Leading Edge Tubercles on Airfoils
  16. Aerodynamic Characteristics of Tubercled Slotted Flaps
  17. Characterization of Tubercle Effects on Finite Span Wings
  18. Euler-based Aerodynamic Shape Optimization of Leading Edge Tubercles in Transonic Flow
  19. Application of Deployable Tubercles as High-Lift Leading-Edge Devices
  20. Further Parametric Investigation of Leading Edge Tubercles on the Propeller Performance
  21. Wake Modelling with Embedded Lateral and Directional Stability Sensitivity Analysis for Aerial Refuelling or Formation Flight
  22. Multi–Objective Design Optimization of an MoM Aircraft using an Asynchronous Constrained PSO
  23. Numerical Study of the Effects of Leading Edge Tubercles on Transonic Performance of Airfoils
  24. Coupled Aircraft Design and Staging Assignment for Long–Range Operations
  25. Effect of Passenger Preferences on the Integrated Design and Optimization of Aircraft Families and Air Transport Network
  26. Effect of Leading Edge Tubercles on Transonic Performance of Airfoils
  27. Analytic study of the conditions required for longitudinal stability of dual-wing aircraft
  28. Coupled Optimization of Aircraft Families and Fleet Allocation for Multiple Markets
  29. Integrated Design and Optimization of Aircraft Families and Air Transport Network
  30. Reynolds Number Effect of Leading Edge Tubercles on Airfoil Aerodynamics
  31. Parametric Study of Box-Wing Aerodynamics for Minimum Drag Under Stability and Maneuverability Constraints
  32. Multidisciplinary Analysis of a Box-Wing Aircraft Designed for a Regional-Jet Mission
  33. Wing weight model for conceptual design of nonplanar configurations
  34. Stability and Control Effects on the Design Optimization of a Box-Wing Aircraft
  35. Coupled Optimization of Aircraft Design and Fleet Allocation with Uncertain Passenger Demand
  36. Coupled Optimization of Aircraft Family Design and Fleet Assignment for Minimum Cost and Fuel Burn
  37. Implementing a Capstone Aircraft Design Project as an Integrated Multi-Disciplinary Development Experience
  38. Sizing of a Short Range Civil Transport Aircraft Considering Aero-Structural and Stability Effects
  39. Effect of Size and Mission Requirements on the Design Optimization of Non-Planar Aircraft Configurations
  40. Aerostructural Optimization of Nonplanar Lifting Surfaces
  41. pyACDT: An Object-Oriented Framework for Aircraft Design Modelling and Multidisciplinary Optimization
  42. Particle Swarm Optimization in Structural Design
  43. Particle swarm approach for structural design optimization
  44. Multidisciplinary Optimization Framework for Control-Configuration Integration in Aircraft Conceptual Design
  45. Relaxed Static Stability Aircraft Design via Longitudinal Control-Configured Multi-disciplinary Design Optimization Methodology
  46. Evaluation of Multidisciplinary Optimization Approaches for Aircraft Conceptual Design
  47. Flight Dynamics and Control Multidisciplinary Integration in Aircraft Conceptual Design Optimization
  48. Early Aircraft and Control Design Integration Through Multidisciplinary Optimization and Surrogate Models
  49. Effective Multi-Mission Aircraft Conceptual Design Optimization Using a Hybrid Multi-Objective Evolutionary Method
  50. Aircraft conceptual design using genetic algorithms