Numerical study of liquid film cooling in a rocket combustion chamber

DOI10.1016/J.IJHEATMASSTRANSFER.2005.06.017zbMath1189.76072OpenAlexW2148648726MaRDI QIDQ981152

J. Martínez

Publication date: 30 June 2010

Published in: International Journal of Heat and Mass Transfer (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ijheatmasstransfer.2005.06.017

Mathematics Subject Classification ID

Thin fluid films (76A20) Combustion (80A25) Reaction effects in flows (76V05)

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Numerical simulation and optimization on heat transfer and fluid flow in cooling channel of liquid rocket engine thrust chamber ⋮ Verification and validation of numerical solutions of two-dimensional reactive flow in rocket engine nozzles

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