Dependency of Surface Temperature on Coolant Mass Flow and Heat Flux in Rocket Combustion Chambers-Reference-Cited by-同舟云学术

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Dependency of Surface Temperature on Coolant Mass Flow and Heat Flux in Rocket Combustion Chambers

Published:2022-03-05 Issue: Volume: Page:
ISSN:
Container-title:2022 IEEE Aerospace Conference (AERO)
language:
Short-container-title:

Author:

Kringe Pascal H.¹,Burger Chris¹,Riccius Jorg R.¹,Zametaev Evgeny¹,Oschwald Michael²,Gernoth Andreas³,Soller Sebastian⁴,Lehmann Marcus⁴,Reese Stefanie⁵

Affiliation:

1. German Aerospace Center, Institute of Space Propulsion,Hardthausen,Germany,74239

2. German Aerospace Center Institute of Space Propulsion & Institute of Jet Propulsion and Turbomachinery, RWTH Aachen University

3. ESA ESTEC,Noordwijk,The Netherlands

4. ArianeGroup GmbH,Munich,Germany

5. Institute of Applied Mechanics, RWTH Aachen University,Aachen,Germany

Funder

European Space Agency

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9843190/9843194/09843694.pdf?arnumber=9843694

Reference32 articles.

1. Multiscale model for turbulent flows

Cited by 1 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. Experimental and Numerical Fatigue Life Study of Inner Liner Material in Rocket Combustion Chambers;2023 IEEE Aerospace Conference;2023-03-04

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