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Published in:

Volume 5 Issue 6
June-2018
eISSN: 2349-5162

Unique Identifier

JETIRC006021

Page Number

114-118

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Title

TO STUDY THE EFFECT OF CANTED ANGLE IN TURBULENCE MIXING IN SUPERSONIC TWIN JET

ISSN

2349-5162

Cite This Article

"TO STUDY THE EFFECT OF CANTED ANGLE IN TURBULENCE MIXING IN SUPERSONIC TWIN JET", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.5, Issue 6, page no.114-118, June-2018, Available :http://www.jetir.org/papers/JETIRC006021.pdf

Abstract

The pressing environmental issue of modern public is jet noise. Air travel is becoming common and affordable globally. The airport authority set endurable limits of jet noise near airports. The review paper concentrate on twin jet interaction, aeroacoustics and fluid flow physics. The computational and experimental investigation on supersonic jet noise is discussed; consist of turbulent mixing noise, screech tones and broadband noise. CFD 2D simulation of axisymmetric converging diverging nozzles of Mach number of 1.76 and canted twin jet has lower turbulence level due to jet interaction in the inter nozzle region. The main objective of this study is to compare the jet structure, turbulence quantities of twinjets and the effect of canted angle in turbulence mixing in supersonic twinjet.

Key Words

Canted twinjet, supersonic nozzle, jet noise, twin jet, Axisymmetric converging diverging nozzles,potential core length, jet interaction, Acoustic shielding

Cite This Article

"TO STUDY THE EFFECT OF CANTED ANGLE IN TURBULENCE MIXING IN SUPERSONIC TWIN JET", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.5, Issue 6, page no. pp114-118, June-2018, Available at : http://www.jetir.org/papers/JETIRC006021.pdf

Publication Details

Published Paper ID: JETIRC006021
Registration ID: 183545
Published In: Volume 5 | Issue 6 | Year June-2018
DOI (Digital Object Identifier):
Page No: 114-118
ISSN Number: 2349-5162

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Cite This Article

"TO STUDY THE EFFECT OF CANTED ANGLE IN TURBULENCE MIXING IN SUPERSONIC TWIN JET", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.5, Issue 6, page no. pp114-118, June-2018, Available at : http://www.jetir.org/papers/JETIRC006021.pdf




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