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- W2051266171 abstract "As a result of 22,000 hr gas turbine engine operation burning residual oil fuels of high sulfur concentration, Inconel-700 blade has been severely affected owing to hot corrosion, whereas Inconel-X has been virtually free from such an attack. Consideration of the alloy composition suggests that molybdenum and cobalt in Inconel-700 and iron in Inconel-X are important elements in relation to hot corrosion. On the basis of metallographic, electron microprobe and X-ray diffraction analyses, the effect of the alloy composition in regard to hot corrosion mechanisms has been discussed in some detail." @default.
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- W2051266171 date "1972-03-26" @default.
- W2051266171 modified "2023-09-23" @default.
- W2051266171 title "Hot Corrosion of Gas Turbine Rotor Blade Materials due to a Long Term Field Testing" @default.
- W2051266171 doi "https://doi.org/10.1115/72-gt-87" @default.
- W2051266171 hasPublicationYear "1972" @default.
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