Computational Analysis On Cold Flow in Swirler by Aerodynamics Properties |
Author(s): |
Amit Kumar , AISECT UNIVERSITY; Mr. Vinay Yadav, AISECT UNIVERSITY |
Keywords: |
Swirler, CFD, recirculation zone |
Abstract |
At mass flow rate of 0.5 kg/s and equivalence ratio are 0.7 to 0.8 ,the cold flow of CFD (computational fluid dynamics )analysis in swirler is done at 400, 500 and 620 are respectively of vane angle. Also find out aerodynamics flow properties in swirler at respective vane angles. At vane angle of 400, 500 and 620, the swirler numbers are 0.6, 0.9 and 1.3 respectively is calculated.So purely CFD analysis of aerodynamics properties of flow in swirler at various mentioned vane angle is investigated and to be designed improvement of swirler with high efficiency of aerodynamics mixing of air and fuel. To support experimental design with CFD analysis will be the key role to predict the improvement of performance and efficiency of swirler. |
Other Details |
Paper ID: IJSRDV4I60067 Published in: Volume : 4, Issue : 6 Publication Date: 01/09/2016 Page(s): 1-3 |
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