Validation and Understanding of UH-60A Vibratory Loads in Steady Level Flight
Validation of Structural and Aerodynamic Modeling Using UH-60A Airloads Program Data
Integrated Trailing-Edge Flaps and Servotabs for Helicopter Primary Control 032005
DESIGN OF SELF-TWISTING ROTOR BLADES FOR HIGH-SPEED COMPOUND ROTORCRAFT (AIAA 2017-0292)
Development of Propulsion System Models for Electric-VTOL Aircraft (AIAA 2018-1750)
FUNDAMENTAL STUDIES OF LITHIUM SULFUR BATTERIES FOR EVTOL AIRCRAFT
AEROMECHANICS OF A COAXIAL MARS HELICOPTER USING HIGH-FIDELITY CFD/CA