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...
Main Authors: | , , |
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Format: | Book |
Language: | English |
Published: |
Penerbit UTM
2012
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Subjects: | |
Online Access: | http://eprints.utm.my/30167/1/MohammadNazriMohd.2012_CombustorAerodynamics.pdf |