Creep damage evolution in a modeling specimen of nickel-based single crystal superalloys air-cooled blades
Plate specimens both with holes and without holes were used to model air-cooled turbine blades. Experimental study on the creep behavior of a second generation nickel-based single crystal has been performed at 980 °C with these modeling specimens in two crystallographic orientations [0 0 1] and [1 1...
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Veröffentlicht in: | Materials science & engineering. A, Structural materials : properties, microstructure and processing Structural materials : properties, microstructure and processing, 2008-03, Vol.477 (1), p.319-327 |
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