All Stories

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