Measurement of Heat Transfer in Liquid Rocket Combustors-Reference-Cited by-同舟云学术

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Measurement of Heat Transfer in Liquid Rocket Combustors

Published:2020-01 Issue: Volume: Page:281-331
ISSN:
Container-title:High-Pressure Flows for Propulsion Applications
language:
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Author:

Oschwald M.,Suslov D.,Haemisch J.,Haidn O.,Celano M.,Kirchberger C.,Rackemann N.,Preu A.,Wiedmann D.

Publisher

American Institute of Aeronautics and Astronautics, Inc.

Reference41 articles.

1. Electrically heated tube investigation of cooling channel geometry effects

Cited by 5 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. Conjugate Heat Transfer Analysis of the Wall Heat Flux in a Liquid Rocket Engine using Wall Models;AIAA SCITECH 2023 Forum;2023-01-19

2. Conjugate Heat Transfer Analysis of the Wall Heat Flux in a Liquid Rocket Engine;AIAA SCITECH 2022 Forum;2022-01-03

3. Wall Heat Flux Evaluation in Regeneratively Cooled Rocket Thrust Chambers;Journal of Thermophysics and Heat Transfer;2021-01

4. Experimental and Numerical Investigation of Heat Transfer Processes in Rocket Engine Cooling Channels Operated with Cryogenic Hydrogen and Methane at Supercritical Conditions;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2021

5. Experimental Investigations of Heat Transfer Processes in Cooling Channels for Cryogenic Hydrogen and Methane at Supercritical Pressure;Lecture Notes in Mechanical Engineering;2020

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