Multi-Domain Modeling for High Temperature Superconducting Components for the CHEETA Hybrid Propulsion Power System
Author:
Affiliation:
1. Rensselaer Polytechnic Institute
2. Ohio State University
3. University of Illinois, Urbana-Champaign
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-3302
Reference10 articles.
1. Initial Steps in Modeling of CHEETA Hybrid Propulsion Aircraft Vehicle Power Systems using Modelica
2. Development and Implementation of a Flexible Model Architecture for Hybrid-Electric Aircraft
3. Simulation of High Temperature Superconductors and experimental validation
4. Quench and stability of Roebel cables at 77 K and self-field: Minimum quench power, cold end cooling, and cable cooling efficiency
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1. Cryogenic turbo-electric hybrid propulsion system with liquid hydrogen cooling for a regional aircraft;International Journal of Hydrogen Energy;2024-06
2. Protection System Architecture for All-Electric Aircraft;IEEE Transactions on Applied Superconductivity;2023-08
3. Electro-Thermal Modeling of Fuel Cells and Batteries for CHEETA Aircraft;AIAA AVIATION 2023 Forum;2023-06-08
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