Numerical investigation of rocket engine cooling channel heat transfer for different LNG under trans-critical conditions-Reference-Cited by-同舟云学术

Numerical investigation of rocket engine cooling channel heat transfer for different LNG under trans-critical conditions

Published:2023-11 Issue: Volume:20 Page:100461
ISSN:2666-2027
Container-title:International Journal of Thermofluids
language:en
Short-container-title:International Journal of Thermofluids

Author:

Nasser Ibraheem,Haidn Oskar,Manfletti Chiara

Funder

Deutsches Zentrum für Luft- und Raumfahrt

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference46 articles.

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3. The case and context for atmospheric methane as an exoplanet biosignature;Thompson;Astronomy,2022

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5. Thermal performance investigation of supercritical methane in minichannel heat sink on flight vehicle actuator under geometry effect of cross section;Gao;Numer. Heat Transfer A,2022

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