Swirl flow combustion -- CFD Online Discussion Forums

September 26, 2018, 05:45	Swirl flow combustion	#1
SUBHANKAR Member subhankar Join Date: May 2016 Posts: 36 Rep Power: 9	How to specify the axial and radial component of flow direction? Does the sum of the above two components of flow direction has to be one? Does it take the tangential velocity into consideration? For example I am giving tangential velocity equal to 1 m/s and the axial and radial components as 0.7 and 0.3 respectively? Are the following specifications correct? If my inlet is an annular cross section revolving around x-axis, then what should be the components of the axis origin?

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