Abstract
Computational investigation of Mach number effects on the combustion zone length in supersonic flow over a ram accelerator has been carried out to provide valuable data for an on-going theoretical study of the same problem. It is found that the combustion zone length is inversely proportional to the Mach number with a significant reduction of about 33% at Mach 3.5 and about 44% at Mach 4, respectively, while comparing to the combustion zone length at Mach 2.5. This correlation provides some useful guidelines to define the control volume box in corresponding theoretical study. © Springer-Verlag Berlin Heidelberg 2009.
Cite
CITATION STYLE
Bengherbia, T., Yao, Y., & Bauer, P. (2009). Effects of Mach number on the combustion zone length for a RAMAC configuration at sub-detonative mode. In Computational Fluid Dynamics 2006 - Proceedings of the Fourth International Conference on Computational Fluid Dynamics, ICCFD 2006 (pp. 689–694). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-3-540-92779-2_108
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