@article{hoglauer_simulation_2013,
	title = {Simulation of {Liquid}, {Transcritical} and {Gaseous} {Cooling} {Films} in {Rocket} {Combustion} {Chambers}},
	abstract = {The focus of the paper is set on the modeling and simulation of liquid, gaseous and transcritical cooling films in rocket combustion chambers. Besides different film fluids such as MMH, NTO, kerosene or methane a major issue is the modeling of films in transcritical state. For the modeling Astrium's in-house code Rocflam-II is applied. The main goal of the used modeling in Rocflam-II is to provide a tool package for the simulation of a wide range of rocket combustion devices, validated against experimental data. This includes the modeling of injection, droplet spray, combustion, wall heat transfer, film cooling as well as additional regenerative cooling simulated by 3D conjugate heat transfer. First successful steps toward this goal are presented in this paper.},
	language = {en},
	author = {Höglauer, Christoph and Kniesner, Björn and Knab, Oliver and Schlieben, Gregor and Haidn, Oskar and Hoeglauer, Christoph},
	year = {2013},
}

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