All Stories

  1. Mid-Fidelity Numerical calculation of XV-15 Proprotor
  2. Preliminary Sizing Correlations for Fixed-Wing Unmanned Aerial Vehicle Characteristics
  3. Fuel cell propulsion in small fixed-wing unmanned aerial vehicles: Current status and research needs
  4. Experimental Testing of Electronic Speed Controllers for UAVs
  5. Derivation of Dual-Switch Step-Down DC/DC Converters With Fault-Tolerant Capability
  6. A Hypersonic Aircraft Optimization Tool with Strong Aerothermoelastic Coupling
  7. Performance of a hybrid, fuel-cell-based power system during simulated small unmanned aircraft missions
  8. Cryogenic hydrogen fuel tanks for large hypersonic cruise vehicles
  9. Analysis of a three-port DC-DC converter for PV-battery system using DISO boost and SISO buck converters
  10. Experimental investigation of the role of the battery in the AeroStack hybrid, fuel-cell-based propulsion system for small unmanned aircraft systems
  11. Impact of heat transfer on the performance of micro gas turbines
  12. Two-transistor step-down DC/DC converters with fault-tolerant capability
  13. Structural Design Optimisation and Aerothermoelastic Analysis of LAPCAT A2 Mach 5 Cruise Vehicle
  14. Development of a Hypersonic Aircraft Design Optimization Tool
  15. Temperature Effect on the Structural Design of a Mach 8 Vehicle
  16. Demonstration of Compact Air Separation Technology for In-Flight Oxygen Collection Space Launchers
  17. Long range transport aircraft using hydrogen fuel
  18. Impact of Heat Transfer on Centrifugal Compressors of Micro Turbines
  19. A Global Experiential Design Studio for Engineering Students
  20. Temperature Effects on Flutter of a Mach 5 Transport Aircraft Wing
  21. Design of a Fuel Cell Powered Blended Wing Body UAV
  22. Structural Design and Optimisation of the LAPCAT A2 Mach 5 Vehicle Based on Aero-Elastic Deformations.
  23. Hyperion UAV: An International Collaboration
  24. Rapid, International Design and Test of a Hybrid-Powered, Blended-Wing Body Unmanned Aerial Vehicle
  25. Workforce Development for Global Aircraft Design
  26. Development of a Mixer Model to Compare Mixed and Unmixed HBPR Turbofans
  27. Comparison of Propulsion Technologies for a HALE Airship
  28. Preliminary Design of an ACES TSTO Air Launch Vehicle