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Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 7, Pp 40-47 (2018)
Interacting between the next rows of the turbine creates a circumferential flow non-uniformity, which leads to origination of resonance dynamic stresses on rotor bladings with frequencies z·fn, where fn - a rotor rotation frequency, z - number of st
Externí odkaz:
https://doaj.org/article/69ca1ee0048548aa96af5ea60ec4f084