Study of flame response to transverse acoustic modes from the LES of a 42-injector rocket engine
Authors:
- A. UrbanoAUA. Urbano
- Q. DouasbinQDQ. Douasbin
- L. SelleLSL. Selle
- G. StaffelbachGSG. Staffelbach
- B. CuenotBCB. Cuenot
- T. SchmittTST. Schmitt
- S. DucruixSDS. Ducruix
- S. CandelSCS. Candel
- 1 January 2017
- journal article
- Published by Elsevier in Proceedings of the Combustion Institute
- Vol. 36 (2) , 2633-2639
Abstract
No abstract availableKeywords
Funding Information
- Deutsches Zentrum für Luft- und Raumfahrt
- European Research Council
- Seventh Framework Programme (ERC-AdG 319067-INTECOCIS, FP/2007-2013)
- Partnership for Advanced Computing in Europe AISBL
- Grand Équipement National De Calcul Intensif
- Centre National d’Etudes Spatiales
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