A Review of Some Early Design Practice Using Computational Fluid Dynamics and a Current Perspective

[+] Author and Article Information
J. H. Horlock, J. D. Denton

Cambridge University Engineering Department, Whittle Laboratory, Madingley Road, Cambridge CB3 0DY, UK

J. Turbomach 127(1), 5-13 (Feb 09, 2005) (9 pages) doi:10.1115/1.1650379 History: Received December 01, 2002; Revised March 01, 2003; Online February 09, 2005
Copyright © 2004 by ASME
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Grahic Jump Location
Axial and tangential lift coefficients of Lakshimarayana’s cascade
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Calculated stagnation pressure contours behind Lakshimarayana’s cascade
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The growth of tip leakage loss through Lakshimarayana’s cascade
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Static pressure contours near the tip of Lakshimarayana’s cascade
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Lift coefficients of the four stages
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Exit flow angles from stage 3, rotor and stator
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(a) Axial velocities at rotor 3 exit, (b) axial velocities at stator 3 exit
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Stagnation pressure contours behind Harrison’s cascade; (a) inviscid calculation with inlet boundary layer, (b) viscous calculation with no inlet boundary layer, (c) viscous calculation with inlet boundary layer, (d) experiment
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Shock pattern in a swept fan. Mach number contours at midpitch.



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