Effect of Inlet and Outlet Manifolds on Regenerative Cooling in LOX/Methane Thrust Chambers
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s11630-020-1312-4.pdf
Reference29 articles.
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5. French A.D., Roncioni P., Comparison of reactive flow simulations for a LOX/CH4 uni-element rocket. 49th AIAA/ASEME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, 2013. DOI: https://doi.org/10.2514/6.2013-4155.
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