@article{(Open Science Index):https://publications.waset.org/pdf/614,
	  title     = {Ignition Time Delay in Swirling Supersonic Flow Combustion},
	  author    = {A. M. Tahsini},
	  country	= {},
	  institution	= {},
	  abstract     = {Supersonic hydrogen-air cylindrical mixing layer is
numerically analyzed to investigate the effect of inlet swirl on
ignition time delay in scramjets. Combustion is treated using detail
chemical kinetics. One-equation turbulence model of Spalart and
Allmaras is chosen to study the problem and advection upstream
splitting method is used as computational scheme. The results show
that swirling both fuel and oxidizer streams may drastically decrease
the ignition distance in supersonic combustion, unlike using the swirl
just in fuel stream which has no helpful effect.},
	    journal   = {International Journal of Aerospace and Mechanical Engineering},
	  volume    = {6},
	  number    = {10},
	  year      = {2012},
	  pages     = {2156 - 2160},
	  ee        = {https://publications.waset.org/pdf/614},
	  url   	= {https://publications.waset.org/vol/70},
	  bibsource = {https://publications.waset.org/},
	  issn  	= {eISSN: 1307-6892},
	  publisher = {World Academy of Science, Engineering and Technology},
	  index 	= {Open Science Index 70, 2012},
	}