Effect of Swirl and Wall Heat Transfer on the Performance of Arcjet Thrusters Using Numerical Modeling-Reference-Cited by-同舟云学术

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Effect of Swirl and Wall Heat Transfer on the Performance of Arcjet Thrusters Using Numerical Modeling

Published:2020-08-01 Issue: Volume: Page:427-447
ISSN:2195-4356
Container-title:Proceedings of the National Aerospace Propulsion Conference
language:
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Author:

Akhare Deepak,Nandyala Hari Prasad,Kumar Amit,Jayachandran T.

Publisher

Springer Singapore

Link

http://link.springer.com/content/pdf/10.1007/978-981-15-5039-3_26

Reference12 articles.

1. Jahn RG (2006) Physics of Electric Propulsion

2. Babu V, Aithal SM, Subramaniam VV (1993) On the effects of swirl in arcjet thruster flows. In: International electric propulsion conference

3. Dutton JC (1987) Swirling supersonic nozzle flow. J Propul Power 3:342–349. https://doi.org/10.2514/3.22996

4. Nguyen-kuok S Theory of Low-temperature plasma physics. n.d

5. Niewood EH (1989) Master of science

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