Modelling and Computational Fluid Dynamic Analysis on Jet Nozzle

Shaik Khaja Hussain , B V Amarnath Reddy , A V Hari Babu

Supersonic nozzle, CFD Analysis solid works.

Supersonic flows associated with missiles, aircraft, missile engine intake and rocket nozzles are often steady. The shape of the nozzle geometry is increasingly attractive in heating, ventilation and air conditioning applications. The objective of the present work is to simulate and understand Supersonic flows with single jet Flow at various Mach numbers. The purpose is to precisely understand the fluid dynamics and variation of flow properties such as velocity, pressure and turbulence in supersonic flow regime for various Mach numbers pressure ratio and dimensionless spacing single jet nozzle. The jet nozzle can take three different materials like Titanium, Tungsten and Nickel. It can observe the material is to be in the supersonic flow in the nozzle. The Mach number at the nozzle exit is observed to be less in comparison with designed value. This is due to the viscosity and turbulence in fluid near the wall of the duct. The Mach number decreases due to shock wave and reversible flow. A single jet nozzle is designed in solidworks software and CFD analysis is carried out in solid works flow simulation.

Published Paper   E-Certificate

"Modelling and Computational Fluid Dynamic Analysis on Jet Nozzle", IJSDR - International Journal of Scientific Development and Research (www.IJSDR.org), ISSN:2455-2631, Vol.1, Issue 9, page no.416 - 425, September-2016, Available :https://ijsdr.org/papers/IJSDR1609066.pdf

Volume 1 Issue 9, September-2016

Pages : 416 - 425

Paper Reg. ID: IJSDR_160835

Published Paper Id: IJSDR1609066

Downloads: 000347059

Research Area: Engineering

Country: nandyal, Andhra Pradesh, India

Published Paper PDF: https://ijsdr.org/papers/IJSDR1609066

Published Paper URL: https://ijsdr.org/viewpaperforall?paper=IJSDR1609066

ISSN: 2455-2631 | IMPACT FACTOR: 9.15 Calculated By Google Scholar | ESTD YEAR: 2016

An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 9.15 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator

Publisher: IJSDR(IJ Publication) Janvi Wave

This work is licensed under a Creative Commons Attribution 4.0 International License and The Open Definition