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Surface roughness of real operationally used compressor blade and blisk

The data set contains three dimensional measured surfaces of real worn compressor blades from real mid-sized air craft engine high pressure coompressors. Three stages of the compressor are measured. The first stage, the centre stage and the last stage.

Also surface data of a real worn Blisk from a small aircraft engine will be published. We are currently preparing the data.

Further information of the data are given in: Gilge, P.; Kellersmann, A.; Friedrichs, J.; Seume J.R. (2019): Surface roughness of real operationally used compressor blade and blisk. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, https://doi.org/10.1177/0954410019843438

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Cite this as

P. Gilge, A. Kellersmann, S. Kurth, F. Herbst, J. Friedrichs and J. R. Seume (2019). Dataset: Surface roughness of real operationally used compressor blade and blisk. https://doi.org/10.25835/0084372

DOI retrieved: 05:22 08 May 2021 (GMT)

Additional Info

Field Value
Author P. Gilge, A. Kellersmann, S. Kurth, F. Herbst, J. Friedrichs and J. R. Seume
Last Updated July 2, 2019, 13:24 (CEST)
Created April 15, 2019, 10:00 (CEST)
License Creative Commons Attribution-NonCommercial 3.0