Status of Experimental Research on High Performance Methane-Fueled Rocket Thrust Chamber-Reference-Cited by-同舟云学术

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Status of Experimental Research on High Performance Methane-Fueled Rocket Thrust Chamber

Published:2011-07-31 Issue: Volume: Page:
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Container-title:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Tomita Takeo,Ueda Shuichi,Kawashima Hidto,Onodera Takuo,Kano Yasuhito,Kubota Isao,Munenaga Takao

Publisher

American Institute of Aeronautics and Astronautics

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. Reduced kinetic mechanism for methane/oxygen rocket engine applications: a reliable and numerically efficient methodology;Combustion Theory and Modelling;2023-01-30

2. Improved Heat-Transfer Correlation for Transcritical Methane Based on a Velocity Profile Correction Term;Journal of Thermal Science and Engineering Applications;2021-07-29

3. Delayed Detached Eddy Simulations with Tabulated Chemistry for Thermal Loads Predictions;Journal of Propulsion and Power;2021-01

4. Effect of Inlet and Outlet Manifolds on Regenerative Cooling in LOX/Methane Thrust Chambers;Journal of Thermal Science;2020-12-03

5. Mechanism and influence factor analysis of heat transfer deterioration of transcritical methane;International Journal of Energy Research;2020-06-23

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