3D INVISCID FLUTTER OF ROTOR BLADES AND STATOR/ROTOR STAGE

Numerical calculations of the 3D transonic flow of an ideal gas through turbomachinery rotor blade row and stator, rotor blades moving relatively one to another with taking into account the blades oscillations are presented.The approach is based edgewater shoes on the solution of the coupled aerodynamic-structure problem for the 3D flow through the

read more