@inproceedings{80c233b004cb40909b21dce4543394ce,
title = "Radiation-based validation of combustion simulations and comparison to heat release in rocket engines",
abstract = "A methodology to predict OH* radiation in turbulent diffusion flames for rocket engine applications with low numerical cost is presented. On the basis of an extended flamelet approach including the OH* species, a RANS combustion simulation for the single injector configuration Mascotte at 60 bar is conducted. For the comparison of the numerical results with experimental radiation data, self-absorption of OH* is accounted for in a post-processing step as well. Results show that the OH* radiation is well reproduced and the consideration of both turbulence-chemistry interaction as well as self-absorption is essential. It is also shown that OH* radiation should not be used to quantify the spatial distribution of the volumetric heat release rate.",
author = "M. Schulze and T. Fiala and T. Sattelmayer",
note = "Publisher Copyright: {\textcopyright} 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All Rights Reserved.; 54th AIAA Aerospace Sciences Meeting, 2016 ; Conference date: 04-01-2016 Through 08-01-2016",
year = "2016",
doi = "10.2514/6.2016-2152",
language = "English",
isbn = "9781624103933",
series = "54th AIAA Aerospace Sciences Meeting",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "54th AIAA Aerospace Sciences Meeting",
}