Modelling Study to Compare the Flow and Heat Transfer Characteristics of Low-Power Hydrogen, Nitrogen and Argon Arc-Heated Thrusters
- ISSN号:1009-0630
- 期刊名称:《等离子体科学与技术:英文版》
- 时间:0
- 分类:TQ116.2[化学工程—无机化工] V439[航空宇航科学与技术—航空宇航推进理论与工程;航空宇航科学技术]
- 作者机构:[1]School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China, [2]Department of Engineering Mechanics, Tsinghua University, Beijing 100084, China, [3]Institute of Mechanics, Chinese Academy of-Sciences, Beijing 100190, China, [4]CSIRO Materials Science and Engineering, Lindfield NSW 2070, Australia
- 相关基金:supported by National Natural Science Foundation of China (Nos. 50836007, 10921062)
关键词:
电弧加热发动机, 超音速流动, 传热特性, 推进器, 氢气, 氮气, 氩气, 电弧喷射推力器, low-power arcjet, plasma flow and heat transfer, numerical modelling,propellant-type effects
中文摘要:
E-mail address of-WANG naixing: whx@buaa.edu.cn