All Stories

  1. Integrated Sizing and Optimization of Aircraft and Subsystem Architectures in Early Design
  2. System-Level Assessment of Active Flow Control for Commercial Aircraft High-Lift Devices
  3. Assessing Impact of Epistemic and Technological Uncertainty on Aircraft Subsystem Architectures
  4. A Simulation-Based Framework for Structural Loads Assessment during Dynamic Maneuvers
  5. Integrated Sizing and Multi-objective Optimization of Aircraft and Subsystem Architectures in Early Design
  6. System-Level Assessment of Active Flow Control for Commercial Aircraft High-Lift Devices
  7. Integrated Assessment of Aircraft and Novel Subsystem Architectures in Early Design
  8. Gas Turbine Transient Response to Subsystem Architecture Secondary Power Off-Takes
  9. Multidisciplinary Approach to Assessing Actuation Power of a Hybrid Wing–Body
  10. Framework for Assessing Impact of Active Flow Control Technologies for Commercial Aircraft
  11. Impact of Subsystem Secondary Power Requirements on Gas Turbine Sizing and Performance
  12. Assessing Impact of Epistemic and Technological Uncertainty on Aircraft Subsystem Architectures
  13. Heuristic Definition, Evaluation, and Impact Decomposition of Aircraft Subsystem Architectures
  14. Integrated Assessment of Aircraft and Novel Subsystem Architectures in Early Design
  15. Method for Evaluating Electrically Actuated Hybrid Wing–Body Control Surface Layouts
  16. Comparative Assessment of Strut-Braced and Truss-Braced Wing Configurations Using Multidisciplinary Design Optimization
  17. An integrated approach to vehicle and subsystem sizing and analysis for novel subsystem architectures
  18. Assessing Taxiing Trade Spaces from Aircraft, Airport, and Airline Perspectives
  19. Pilot-Friendliness Considerations for Personal Air Vehicle Flight Control Systems
  20. Effect of Major Subsystem Power Off-takes on Aircraft Performance in More Electric Aircraft Architectures
  21. Integrating Subsystem Sizing into the More Electric Aircraft Conceptual Design Phase
  22. Uncertainty Quantification for the Actuation Power Requirements of a Hybrid Wing Body Configuration with Electrically Actuated Flight Control Surfaces
  23. Multidisciplinary Design Optimization of a Truss Braced Wing Concept
  24. Analysis of the Effect of Cruise Speed on Fuel Efficiency and Cost for a Truss-Braced Wing Concept
  25. Assessment of Electrically Actuated Redundant Control Surface Layouts for a Hybrid Wing Body Concept
  26. A Preliminary Study of High Lift System Design and Actuation for a Personal Air Vehicle Concept
  27. A Requirements-driven Methodology for Integrating Subsystem Architecture Sizing and Analysis into the Conceptual Aircraft Design Phase
  28. A System and Mission Level Analysis of Electrically Actuated Flight Control Surfaces using Pacelab SysArc