An efficient modeling framework for wall heat flux prediction in rocket combustion chambers using non adiabatic flamelets and wall-functions
In this work an efficient numerical framework for the prediction of wall heat loads in Liquid
Rocket Engine combustion chambers is presented. The proposed framework is based on a …
Rocket Engine combustion chambers is presented. The proposed framework is based on a …
[PDF][PDF] Simulations of turbulent combustion and wall heat transfer in single and multi injectors GCH4/GOx rocket combustors
G Indelicato, PE Lapenna, D Durigon… - 8th European Conference …, 2019 - eucass.eu
In the present work a methodology is proposed for the modelization of wall heat fluxes within
operative rocket combustion chamber conditions. It is based on a newly developed non …
operative rocket combustion chamber conditions. It is based on a newly developed non …