Open AccessLarge-Eddy Simulations of a sub-scale liquid rocket combustor: influence of fuel injection temperature on thermo-acoustic stability
Author(s) -
Thomas Schmitt,
Gabriel Staffelbach,
Sébastien Ducruix,
Stefan Gröning,
Justin Hardi,
Michael Oschwald
Publication year - 2017
Publication title -
hal (le centre pour la communication scientifique directe)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.13009/eucass2017-352
Subject(s) - combustor , liquid propellant rocket , rocket (weapon) , combustion , aerospace engineering , coaxial , liquid oxygen , large eddy simulation , combustion chamber , rocket engine , materials science , nuclear engineering , hydrogen , mechanics , mechanical engineering , propellant , engineering , physics , turbulence , chemistry , oxygen , organic chemistry , quantum mechanics