What is it about?
We show experimental results of a bladed disk experiencing synchronous vibrations and present a parametric reduced order modeling method to efficiently model the system mistuning and rotational speed. The computational results are compared to the experimental results, showing good agreement.
Featured Image
Read the Original
This page is a summary of: Experimental Investigation of Bladed Disk Dynamics at Design Speed Under Synchronous Vibration, AIAA Journal, October 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059827.
You can read the full text:
Contributors
The following have contributed to this page
