• Sivaram M
• Deepak Joshi
• C P Anand
• Prabu T

The main objective is to analyze a C-D nozzle to understand the phenomena of various design conditions with divergent angles 5°,10°, 15°, 20° by Computational Fluid Dynamic (CFD) The target of this paper is to concentrates at the variety of parameters like velocity, Total pressure, turbulence intensity, and all-out temperature in the four different divergent angle of the nozzles, CFD methodology is implemented in the ANSYS-Fluent Software with K-Epsilon Turbulence equations, and get the results of increase in divergent angle the performance of the nozzle is increased.

C-D Nozzle, Divergent Angle, CFD, ANSYS-Fluent

"CFD ANALYSIS OF ROCKET NOZZLE WITH VARIOUS ANGLE OF DIVERGENCE USING ANSYS-FLUENT SOFTWARE", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.833-839, June-2019, Available :http://www.jetir.org/papers/JETIR1906D30.pdf

"CFD ANALYSIS OF ROCKET NOZZLE WITH VARIOUS ANGLE OF DIVERGENCE USING ANSYS-FLUENT SOFTWARE", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp833-839, June-2019, Available at : http://www.jetir.org/papers/JETIR1906D30.pdf