All Stories

  1. Statistical Wind-Tunnel Experimentation Advancements for eVTOL Aircraft Aero-Propulsive Model Development
  2. Experimental Characterization of an Electric Ducted Fan for the SUSAN 25% Scale Research Vehicle
  3. Development and Evaluation of Multirotor Flight Dynamic Models for Estimation and Control
  4. System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data
  5. Aero-Propulsive Modeling for Propeller Aircraft Using Flight Data
  6. Aero-Propulsive Modeling for eVTOL Aircraft Using Wind Tunnel Testing with Multisine Inputs
  7. Efficient Variable-Pitch Propeller Aerodynamic Model Development for Vectored-Thrust eVTOL Aircraft
  8. Aero-Propulsive Modeling for Tilt-Wing, Distributed Propulsion Aircraft Using Wind Tunnel Data
  9. System Identification for Propellers at High Incidence Angles
  10. Rapid Aero Modeling for Urban Air Mobility Aircraft in Wind-Tunnel Tests
  11. Wind Tunnel-Based Aerodynamic Model Identification for a Tilt-Wing, Distributed Electric Propulsion Aircraft
  12. System Identification for Propellers at High Incidence Angles
  13. Wind Tunnel Testing Techniques for a Tandem Tilt-Wing, Distributed Electric Propulsion VTOL Aircraft
  14. Rapid Aero Modeling for Urban Air Mobility Aircraft in Computational Experiments
  15. Intelligent Contingency Management for Urban Air Mobility
  16. Nonlinear Model Identification Methodology for Small, Fixed-Wing, Unmanned Aircraft