Numerical reduction of dynamic model matrices of aero-engine bladed discs
Research Groups LAQ AerMec per componenti di turbine e compressori
Thesis type NUMERICAL AND DESIGN ORIENTED
Description A FE model of a simple bladed disk will be proposed to which a recently developed new reduction technique (SMART) will be applied to reduce the matrices for calculating the dynamic response of the disk.
The thesis will consist in the application of the SMART technique using ANSYS to generate the model and the necessary data, and matlab to apply the reduction technique.
The codes written in matlab are already available.
Required skills A good knowledge of Matlab and possibly a basic knowledge of Ansys is requested.
Deadline 31/12/2023 PROPONI LA TUA CANDIDATURA