Lithium–Ion Battery Modeling for Aerospace Applications
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036209
Reference43 articles.
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2. Optimization of Commercial Aircraft Using Battery-Based Voltaic-Joule/Brayton Propulsion
3. Optimal Airspeeds for Scheduled Electric Aircraft Operations
4. Optimal Battery Weight Fraction for Maximum Aircraft Range and Endurance
5. Preliminary Sizing Method for Hybrid-Electric Distributed-Propulsion Aircraft
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