The numerical analysis of aeroelastic behaviour of blade row in stage and a half compressor stage
DOI:
https://doi.org/10.15587/1729-4061.2011.1663Keywords:
3D ideal flow, blade rowAbstract
The partial integration method has been used to numerical modelling of the unsteady loads and aeroelastic oscillations of the compressor blade row in 3D ideal gas flow with taking into account the stator S0 – rotor RK – stator S1 aerodynamic interactionReferences
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