Considering Turbofan Operability in Hybrid Electric Aircraft Propulsion System Design
Modeling Turboshaft Engines for the Revolutionary Vertical Lift Technology Project, Expanded
Progress in aircraft gas turbine engine development.
Optimization of Turbine Engine Cycle Analysis with Analytic Derivatives
Exploring Propulsion System Requirements for More and All-Electric Helicopters
Design Exploration of a Mild Hybrid Electrified Aircraft Propulsion Concept