CFD Analysis of a Rocket Nozzle withFour Inlets at Mach 2.1.
Journal Title: International Journal of Science Engineering and Advance Technology - Year 2016, Vol 4, Issue 2
Abstract
In this work CFD investigation of weight and temperature for a rocket spout with four channels at Mach 2.1 is examined with the assistance of familiar programming. at the point when the fuel and air enter in the ignition chamber as indicated by the x and y plot, it is smoldering because of high speed and temperature and afterward temperature increments quickly in burning chamber and joined a portion of the spout and after that temperature diminishes in the way out some portion of the spout. it is deduced in this paper Four gulf rocket spout is having preferred execution over single channel and two delta as seen from the past exploration work done.
Authors and Affiliations
Parasa Lakshmana Kumar| PG Scholar, Pydah College of Engineering, Kakinada, AP, India, G. Sreenivas| Associate Professor, Pydah College of Engineering, Kakinada, AP, India
Keywords
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- EP ID EP16731
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