Comparison of Supersonic Nozzles in Different Outlet Divergence Angle using CFD |
Author(s): |
| Jyoti Kumari , screm; CS Koli, SCREM |
Keywords: |
| CFD, Supersonic Nozzles |
Abstract |
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The comparative flow analysis on the supersonic nozzle has been performed by this experiment. The experiment is done with same parameters like inlet, outlet and length of nozzle but different throat angles. The first throat angle or outlet divergent angle is 10°and second outlet divergent angle (throat angle) is 20°. The experiment has been set on the two prefatory steps. Modelling and CFD analysis are including and after that comparing their different properties of the nozzle. The two dimensional axisymmetric supersonic nozzles were drawn in design modeler of ANSYS WORKBENCH 14.5 and CFD analysis is done on the fluent. The cross sectional area of inlet and outlet are same, throat area and nozzles length are exactly same. At the end of this experiment, analyzing the velocity, pressure, temperature behavior on the nozzles and to take final results. |
Other Details |
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Paper ID: IJSRDV4I110408 Published in: Volume : 4, Issue : 11 Publication Date: 01/02/2017 Page(s): 446-449 |
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