Abstract: The mistuning effects on the aeroelastic stability of axial compressor rotor blades have been investigated by employing aeroelastic eigenvalue method. An axial compressor rotor suffered from flutter failure has been analyzed ...

Abstract: The tip clearance effects on aeroelastic stability of axial compressor blades are investigated with two independent threedimensional (3D) flutter prediction approaches: energy method and aeroelastic eigenvalue analysis. ...