A Subscale-Based Life Prediction Methodology for Rocket Engine Combustor-Reference-Cited by-同舟云学术

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A Subscale-Based Life Prediction Methodology for Rocket Engine Combustor

Published:2003-06-26 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

Sung In-Kyung¹,Northcutt Brett¹,Rubel Ken¹,Anderson William¹

Affiliation:

1. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4900

Reference10 articles.

1. Experimental fatigue life investigation of cylindrical thrust chambers

2. Jankovsky, R.S., Arya, V. K., Kazaroff, J.M., Halford, G.R. "Structurally Compliant Rocket Engine Combustion Chamber-Experimental and AnalyticalValidation,"NASA TP3431,1994.

3. Kasper, H. J. "Thrust Chamber Life Prediction", NASACP-2372,pp36-43,1984.

Cited by 3 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. Wall heat flux measurements in a GO₂/GH₂ heat-sink combustion chamber;Journal of Thermal Science and Technology;2018

2. The Propulsion Program in the School of Aeronautics and Astronautics at Purdue;53rd AIAA/SAE/ASEE Joint Propulsion Conference;2017-07-07

3. A Subscale-Based Rocket Combustor Life Prediction Methodology;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

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