Journal of Failure Analysis and Prevention

, Volume 8, Issue 5, pp 482–482 | Cite as

Stress-Rupture Characterization in Nickel-Based Superalloy Gas Turbine Engine Components

  • Wesley D. PridemoreEmail author
Erratum Technical Article---Peer-Reviewed

Erratum to: J Fail. Anal. and Preven. DOI 10.1007/s11668-008-9140-y

Due to a publication error, Figure 15 was published with the labels switched for the two micrographs. We apologize for this error, and print the corrected Figure 15 below.
Fig. 15

Effect of high-temperature exposure resulting in partial resolutioning of the gamma prime (γ′) precipitates in a SX blade casting. Rafting (coalescence and elongation of the γ′) occurs perpendicular to the primary stress direction. Cuboidal precipitates (darker phase) is γ′. Matrix is the lighter γ phase. Etchant: 33% glycerol, 33% nitric acid, 33% acetic acid, and 1–3% hydrofluoric acid

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© ASM International 2008

Authors and Affiliations

  1. 1.Failure Analysis, Materials, Processes and Engineering DepartmentCincinnatiUSA

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