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Errata

Erratum: “Influence of Blade Deterioration on Compressor and Turbine Performance” [Journal of Engineering for Gas Turbines and Power, 2010, 132(3), p. 032401] OPEN ACCESS

[+] Author and Article Information
M. Morini, M. Pinelli, P. R. Spina, M. Venturini

J. Eng. Gas Turbines Power 132(11), 117001 (Aug 05, 2010) (3 pages) doi:10.1115/1.4001765 History: Published August 05, 2010; Online August 05, 2010
FIGURES IN THIS ARTICLE

The correct form of the equation which defines ηC (reported on p. 10, first column, line 2 of the printed version) is the following:

ηC=h(T0(n+1)s)h(T01)h(T0(n+1))h(T01)

Moreover, in the published paper, there are several mismatches between captions and figures for Figs.  234 and  7891011. The correct coupling between captions and figures is reported in the following.

Copyright © 2010 by American Society of Mechanical Engineers
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References

Figures

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Figure 2

Effect of fouling on the first compressor stage (ΔA*=−10%,Δη*=−5%)

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Figure 3

Effect of gradual fouling on all stages

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Figure 4

Effect of fouling on the whole compressor (ΔA*=−10%,Δη*=−5%)

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Figure 7

Effect of fouling on turbine first stator (ΔA*=−6%,ΔY*=+3%)

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Figure 8

Effect of gradual fouling on the whole turbine

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Figure 9

Effect of fouling on the whole turbine (ΔA*=−6%,ΔY*=+3%)

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Figure 10

Effect of erosion on turbine first stator (ΔA*=+6%)

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Figure 11

Effect of erosion on the whole turbine (ΔA*=+6%)

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