Hot-Gas-Side Heat Transfer Characteristics of a Ribbed Combustor-Reference-Cited by-同舟云学术

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Hot-Gas-Side Heat Transfer Characteristics of a Ribbed Combustor

Published:2009-08-02 Issue: Volume: Page:
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Container-title:45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Kawashima Hideto,Sakamoto Hiroshi,Takahashi Mamoru,Sasaki Masaki,Kumakawa Akinaga

Publisher

American Institute of Aeronautics and Astronautics

Reference3 articles.

1. 1Kumakawa, A., Moriya, S., Tadano, M., Sato, Masahiro. Sato, Masaki. Kusaka, K., Hasegawa, K., and Takahashi, H. "Research about heat load control to combustor inner wall," Proceedings of The Japan Society for Aeronautical and Space Sciences NorthernBranchmeeting 2004 and5thReusableSpacePropulsionSymposium,2004,pp.156-161

Cited by 4 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. Comparative Analysis of Heat Flux Variation in LOx/GCH₄ Ribbed Combustor with Different Rib Types;AIAA SCITECH 2024 Forum;2024-01-04

2. Numerical Evaluation of Heat Transfer Enhancement in Rocket Thrust Chambers by Wall Ribs;Numerical Heat Transfer, Part A: Applications;2014-06-04

3. Numerical Simulation of Hot-Gas Side Heat Transfer Enhancement in Thrust Chambers by Wall Ribs;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

4. Heat Flux Evaluation in Oxygen/Methane Thrust Chambers by RANS Approach;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25

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