Aircraft Design

Performance Assessment of a Distributed Electric Propulsion System for a Medium Altitude Long Endurance Unmanned Aerial Vehicle
An Update on Sizing and Performance Analysis of a Hybrid Turboelectric Regional Jet for the NASA ULI Program
Feasibility Assessments of a Hybrid Turboelectric Medium Altitude Long Endurance Unmanned Aerial Vehicle
A Methodology For Dynamic Sizing of Electric Power Generation and Distribution Architectures
Sizing and Optimization of Novel General Aviation Vehicles and Propulsion System Architectures
A Methodology for Sizing and Analysis of Electric Propulsion Subsystems for Unmanned Aerial Vehicles