An Electrical Modeling and Thermal Analysis Toolbox for Electrified Aircraft Propulsion Simulation
Author:
Affiliation:
1. HX5, LLC
2. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. Aeropropulsive Interaction and Thermal System Integration within the ECO-150: A Turboelectric Distributed Propulsion Airliner with Conventional Electric Machines
2. Conceptual Design of a Single-Aisle Turboelectric Commercial Transport with Fuselage Boundary Layer Ingestion
3. VTOL Urban Air Mobility Concept Vehicles for Technology Development
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1. System Health Management for a Series/Parallel Partial Hybrid Powertrain with Distributed Electric Propulsion;AIAA SCITECH 2024 Forum;2024-01-04
2. Comparison of the Electrical Modeling and Thermal Analysis Toolbox Physics Based Model Blocks to Electrified Aircraft Propulsion Motor Test Hardware;AIAA AVIATION 2023 Forum;2023-06-08
3. Flight Simulator Demonstration of Powertrain Failure Mitigation in a Partial Turboelectric Aircraft;AIAA AVIATION 2023 Forum;2023-06-08
4. Thermal Management System Optimization for a Parallel Hybrid Aircraft Considering Mission Fuel Burn;Aerospace;2022-04-26
5. Implementation Approach for an Electrified Aircraft Concept Vehicle in a Research Flight Simulator;AIAA SCITECH 2022 Forum;2022-01-03
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