All Stories

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