An efficient modeling framework for wall heat flux prediction in rocket combustion chambers using non adiabatic flamelets and wall-functions-Reference-Cited by-同舟云学术

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An efficient modeling framework for wall heat flux prediction in rocket combustion chambers using non adiabatic flamelets and wall-functions

Published:2021-04 Issue: Volume:169 Page:120913
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Indelicato G.^ORCID,Lapenna P.E.,Remiddi A.^ORCID,Creta F.^ORCID

Publisher

Elsevier BV

Subject

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

Reference79 articles.

1. Prometheus, a low cost LOX/CH4 engine prototype;Iannetti,2017

2. Development of LM10-MIRA liquid oxygen–liquid natural gas expander cycle demonstrator engine;Bellomi;Progress in Propulsion Physics,2019

3. The HYPROB LOX-LCH4 demonstrator: status of the manufacturing and experimental activities;Battista,2017

4. Conceptual investigations for a methane-fueled expander rocket engine;Brown,2004

5. History of liquid propellant rocket engines;Sutton,2005

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