All Stories

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