Combustor aerodynamics

Combustor aerodynamics

This book describes the new innovation of gas turbine swirler. The novel swirler is a multiple entry swirler which allows the swirl number to vary on the same value of Reynolds number, by regulating the ratio between the axial and tangential flow momentum. Three–dimensional turbulence and isothermal...

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Bibliographic Details
Main Authors:	Mohd. Jaafar, Mohammad Nazri, Mat Lazim, Tholudin, A. Eldrainy, Yehia
Format:	Book
Language:	English
Published:	Penerbit UTM 2012
Subjects:	TJ Mechanical engineering and machinery
Online Access:	http://eprints.utm.my/30167/1/MohammadNazriMohd.2012_CombustorAerodynamics.pdf

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