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The design of a test rig for the investigation of turbine blade internal cooling channel configurations under the influence of rotation is presented. Rotational speeds of up to 900rpm in combination with the possibility to operate the test model with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::c58d411290caa2638aa10f15eb0030b1
https://hal.archives-ouvertes.fr/hal-01884257
https://hal.archives-ouvertes.fr/hal-01884257
