This paper is published in Volume 3, Issue 10, 2018
Area
Thermal Engineering
Author
Uttam Kumar
Co-authors
Sudhir Singh Rajput, Dr. Praveen Borkar
Org/Univ
Raipur Institute of Technology, Raipur, Chhattisgarh, India
Pub. Date
01 October, 2018
Paper ID
V3I10-1137
Publisher
Keywords
CFD (Computational Fluid Dynamic), CVM (Control Volume Method), DC (Divergent Convergent Nozzle)

Citationsacebook

IEEE
Uttam Kumar, Sudhir Singh Rajput, Dr. Praveen Borkar. CFD analysis and parameter optimization of Divergent Convergent Nozzle, International Journal of Advance Research, Ideas and Innovations in Technology, www.IJARnD.com.

APA
Uttam Kumar, Sudhir Singh Rajput, Dr. Praveen Borkar (2018). CFD analysis and parameter optimization of Divergent Convergent Nozzle. International Journal of Advance Research, Ideas and Innovations in Technology, 3(10) www.IJARnD.com.

MLA
Uttam Kumar, Sudhir Singh Rajput, Dr. Praveen Borkar. "CFD analysis and parameter optimization of Divergent Convergent Nozzle." International Journal of Advance Research, Ideas and Innovations in Technology 3.10 (2018). www.IJARnD.com.

Abstract

The current research work is related to the computational fluid dynamic analysis of two-dimensional convergent-divergent nozzle in Ansys software. It using the CVM (control volume method) to solve the governing equation of fluid flow problem formulated under the given boundary condition. The basic aim of the current study is to determine the most suitable or optimum configuration of convergent-divergent angle in DC Nozzle. The parameter of a nozzle is taken according to the DC nozzle geometry. The different configuration has made by vary angle from 15 to 40 degree at the step of 5 degrees for Convergent angle and for divergent angle, it varies from 12.5 degrees to 20 degrees at the step of 2.5 degrees. The analysis was performed in the fluent workbench of ansys software. The input data for the nozzle is taken as the temperature of exhaust gas and pressure at the inlet. The output data is obtained by fluent in the form of temperature plot and pressure distribution and velocity gradient and Mach number are calculated for each combination.
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