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In many cases, performing material tests of damages in aviation structure elements requires analysing similar problems in specifi c construction elements. This article describes two similar cases of damages in compressor disks made of titanium alloys. In the article examined elements are presented, as well as nature of their damages. Moreover, the article discusses applied test methods and how tests were performed. Included in the article test results analysis leads to identifi cation of the causes of the damages.

Selected problems of material testing of damaged compressor disks made of titanium alloys