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This paper presents the compressor blade algorithm for predicting the defect influence on the characteristics of the stage, axial compressor or GTU as a whole. Based on the description of the topology of the blade profile geometry, an algorithm for c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od_______917::07b24aa7655b59a0628f6361b720f5d1
https://hdl.handle.net/10995/106237
https://hdl.handle.net/10995/106237
