Single shaft gas turbine engine rotor dynamic stresses determination
Date Issued
2025
Author(s)
Smetankina Natalia
Morhun Serhii
Abstract
The problem of the gas turbine rotor dynamic stresses determination has been studied. The developed mathematical model takes into account the curvilinear finite elements of hexagonal type. The turbine rotor dynamic stresses fields were found for several most dangerous forced vibration modes and proved experimentally.
