Using Multi-physics System Simulation to Predict Battery Pack Thermal Performance and Risk of Thermal Runaway During eVTOL Aircraft Operations-Reference-Cited by-同舟云学术

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Using Multi-physics System Simulation to Predict Battery Pack Thermal Performance and Risk of Thermal Runaway During eVTOL Aircraft Operations

Published:2019-08-16 Issue: Volume: Page:
ISSN:
Container-title:AIAA Propulsion and Energy 2019 Forum
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Author:

Harrison Jonathan¹,Charles Devin²,Zenker Jon¹,Frank Evan²

Affiliation:

1. Gamma Technologies, LLC

2. Airbus

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. Trajectory Optimization of Electric Aircraft Subject to Subsystem Thermal Constraints

2. Performance Metrics Required of Next-Generation Batteries to Electrify Vertical Takeoff and Landing (VTOL) Aircraft

Cited by 14 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Optimized design of liquid-cooled plate structure for flying car power battery system;Journal of Energy Storage;2024-09

2. Design and In-Flight Analysis of an Electric Aircraft’s Battery Thermal Management System;2024 IEEE Transportation Electrification Conference and Expo (ITEC);2024-06-19

3. Optimisation of a liquid cooling system for eVTOL aircraft: Impact of sizing mission and battery size;Applied Thermal Engineering;2024-06

4. Novel battery power capability assessment for improved eVTOL aircraft landing;Applied Energy;2024-05

5. Initial Current Discrepancy in Simulating Lithium-Ion Battery Packs - Resolution from Dr. Ralph White’s Analytical Approach;Journal of The Electrochemical Society;2023-10-01

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