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Errata

Erratum: “Low-Speed Model Testing Studies for an Exit Stage of High Pressure Compressor” [ASME Journal of Engineering for Gas Turbines and Power, 2014, 136(11), p. 112603, DOI: 10.1115/1.4027637]

J. Eng. Gas Turbines Power 136(12), 127001 (Jun 27, 2014) (1 page) Paper No: GTP-14-1252; doi: 10.1115/1.4027784 History: Received May 28, 2014; Revised May 29, 2014

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References

Figures

Grahic Jump Location
Fig. 13

Normalized absolute pressure contours for inlet and exit planes of the model stage

Grahic Jump Location
Fig. 12

Absolute Mach number contours for inlet and exit planes of the model stage

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