System-level Utilization of Low-grade, MW-scale Thermal Loads for Electric Aircraft
Author:
Affiliation:
1. Massachusetts Institute of Technology
2. University of Illinois at Urbana-Champaign
3. The Pennsylvania State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3291
Reference26 articles.
1. Hybrid Electric Aircraft Battery Heat Acquisition System
2. Fuel Cell Systems for Aircraft Application
3. Conceptual Design of Distributed Electrified Boundary Layer Ingesting Propulsors for the CHEETA Aircraft Concept
4. Design and Simulation of a Commercial Hybrid Electric Aircraft Thermal Management System
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