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TECHNICAL PAPERS

An Implicit Fluctuation Splitting Scheme for Turbomachinery Flows

[+] Author and Article Information
A. Bonfiglioli

DIFA Università della Basilicata, Contrada Macchia Romana, 85100 Potenza, Italyemail: bonfiglioli@unibas.it

P. De Palma, G. Pascazio, M. Napolitano

DIMeG and CEMeC, Politecnico di Bari, via Re David, 200, 70125 Bari, Italy

J. Turbomach 127(2), 395-401 (May 05, 2005) (7 pages) doi:10.1115/1.1777576 History: Received April 15, 2004; Revised April 17, 2004; Online May 05, 2005
Copyright © 2005 by ASME
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References

Figures

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Defninition of inflow and outflow points
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Nonlinear scheme configurations
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Local view of the coarse grid at the leading edge
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Convergence histories for the M2,is=0.81 case
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Coarse grid: Mach number contours for M2,is=0.81(ΔM=0.05)
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Fine grid: Mach number contours for M2,is=0.81(ΔM=0.05)
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Coarse grid: Mach number contours for M2,is=1(ΔM=0.05)
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Isentropic Mach number distributions along the blade for M2,is=0.81
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Isentropic Mach number distributions along the blade for M2,is=1
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Isentropic Mach number distributions along the blade for M2,is=1.11
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Isentropic Mach number distributions along the blade for M2,is=1.2
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Fine grid: Mach number contours for M2,is=1.2(ΔM=0.05)
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Coarse grid: Mach number contours for M2,is=1.2(ΔM=0.05)
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Fine grid: Mach number contours for M2,is=1.11(ΔM=0.05)
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Fine grid: Mach number contours for M2,is=1(ΔM=0.05)
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Coarse grid: Mach number contours for M2,is=1.11(ΔM=0.05)

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