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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
Design and Analysis of the Thermal Management System of a Hybrid Turboelectric Regional Jet for the NASA ULI Program
Feasibility Assessments of a Hybrid Turboelectric Medium Altitude Long Endurance Unmanned Aerial Vehicle
Transient Surrogate Modeling for Thermal Management Systems
Sizing and Optimization of Novel General Aviation Vehicles and Propulsion System Architectures
Development of Parametric Power Generation and Distribution Subsystem Models at the Conceptual Aircraft Design Stage
Sizing, integration and performance evaluation of hybrid electric propulsion subsystem architectures
A Methodology for Sizing and Analysis of Electric Propulsion Subsystems for Unmanned Aerial Vehicles
A Multi-Disciplinary Integrated Design Environment for Requirements Development and Performance Evaluation of Autonomous Systems