doi: 10.7763/IJCEA.2010.V1.55
CFD Analysis of a Rocket Nozzle with FourInlets at Mach 2.1
K. M. Pandey1
,
- 1Department of Mechanical Engineering, N.I.T Silchar, Assam, India.
- 2Department of Mechanical Engineering,Gurgaon Engineering College, Gurgaon.
Abstract
In this paper CFD analysis of pressure and temperature for a rocket nozzle with four inlets at Mach 2.1 is analyzed with the help of fluent software. when the fuel and air enter in the combustion chamber according to the x and y plot, it is burning due to high velocity and temperature and then temperature increases rapidly in combustion chamber and convergent part of the nozzle and after that temperature decreases in the exit part of the nozzle. it is concluded in this paper that Four inlet rocket nozzle is having better performance than single inlet and two inlet as seen from the previous research work done.
How to Cite
K. M. Pandey and S. K. Yadav, "CFD Analysis of a Rocket Nozzle with FourInlets at Mach 2.1," International Journal of Chemical Engineering and Applications, vol. 1, no. 4, pp. 319-325, 2010. https://doi.org/10.7763/IJCEA.2010.V1.55
Copyright & License
Copyright © 2010 by the authors. This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited (CC BY 4.0).
