All Stories

  1. Probabilistic Optimization of a Hybrid-Electric Canard-Wing General Aviation Aircraft
  2. Control Law Development, Flight Testing, and System Identification of a Distributed Electric Propulsion Subscale Aircraft
  3. Extending an Automated Methodology for Simulation Model Calibration to Manufacturer and Flight Test Validation Data
  4. Flight-Testing of the VT-03-s Shadow Multi-Tilt-Rotor Configuration in VTOL and CTOL Operations
  5. Uncertainty Quantification in the Conceptual Design of Hybrid-Electric General Aviation Aircraft
  6. Sizing and Optimization of a Subscale VTOL Aircraft with COTS Components Using the PEACE Framework
  7. Integrating Strip-Theory Aerodynamics Into Conceptual Design of Variable Geometry Swing-Wing Aircraft
  8. Assessment of Liquid Hydrogen Propulsion System Architectures for a Blended Wing Body Concept
  9. Sizing and Analysis of Hybrid-Electric Single Main Rotor NOTAR Helicopters using the PEACE Framework
  10. Developing Flight Simulation Model for a Lift-Plus-Cruise Subscale Vehicle: Mass Properties, Propulsion, and System Identification
  11. Integrating Flight Dynamics Constraints Into the Conceptual Design of a Vectored Thrust UAM Vehicle
  12. Extension of a Full Envelope Flight Control System to CTOL/STOL Capabilities on a Urban Air Mobility Tilt-Rotor
  13. Comparing Mass Properties and Manufacturability of 3D-Printed and Balsa Subscale Lift-Plus-Cruise Aircraft Designs
  14. Towards an Automated Methodology for Simulation Model Calibration to Manufacturer and Flight Test Performance Data
  15. Sizing and Optimization of Multi eVTOL Configuration for Urban Air Mobility Applications
  16. Development and Testing of a Hybrid Electric Propulsion Architecture for Subscale eVTOL
  17. Sizing and Analysis of Canard-Wing Aircraft With Jet Propulsion
  18. Flight Testing of a Simplified Vehicle Operations Flight Control System on a Subscale Lift-Plus-Cruise Unmanned Air Vehicle
  19. Flight Dynamics and Control Integration in Conceptual Design of an Advanced Air Mobility VTOL Aircraft
  20. Piloted Simulation-Based Assessment of Simplified Vehicle Operations for Urban Air Mobility
  21. Design, Control Law Development, and Flight Testing of a Subscale Lift-Plus-Cruise Aircraft
  22. Integrating Stability and Control Considerations into the Sizing of an Advanced Air Mobility VTOL Aircraft
  23. Optimizing the Design and Subsystems Architecture of an Advanced Air Mobility Aircraft
  24. Electrified Lift-Plus-Cruise Aircraft Sizing with Varying Battery Modeling Assumptions
  25. Design and Sizing of an Electrified Lift-Plus-Cruise Ducted Fan Aircraft
  26. Sizing and Analysis of a Lift-Plus-Cruise Aircraft with Electrified Propulsion
  27. Sizing of Tilt-Wing Aircraft with All-Electric and Hybrid-Electric Propulsion
  28. Sizing and Analysis of a Lift-Plus-Cruise VTOL Aircraft with Electrified Propulsion Systems
  29. Total Energy Based Flight Control System Design for a Lift-Plus-Cruise Urban Air Mobility Concept
  30. A Generalized Energy-Based Vehicle Sizing and Performance Analysis Methodology
  31. Generalized Energy-Based Flight Vehicle Sizing and Performance Analysis Methodology
  32. Aircraft Performance Model Calibration and Validation for General Aviation Safety Analysis
  33. A Simulation-Based Structural Loads Assessment Framework - Application to Symmetric Maneuvering Conditions
  34. Data-Driven General Aviation Aircraft Performance Modeling and Safety Research
  35. A Reconfigurable Flight Simulation Framework Aimed at Novel Flight Vehicle Concepts
  36. Development of A Certification Module for Early Aircraft Design
  37. Development of a Modeling, Flight Simulation, and Control Analysis Capability for Novel Vehicle Configurations
  38. Aero-Propulsive Analysis for Contemporary Conceptual Design
  39. Energy-Based Sizing and Mission Performance Analysis Approach for Novel Flight Vehicle Concepts
  40. Design Overview of the Hexa-Chakra Electric Vertical Takeoff and Landing Personal Air Vehicle