Abstract
Experiments on disk flutter of hard disk drives with non-uniform gap between disks and a shroud were conducted. In this experiments, polyester tapes were partly attached on the shroud so that the shroud gap was changed along the circumference of the disks. Three non-axisymmetric normal modes of the disk were measured, and these amplitude had extremal values at the circumferential position where the shroud gap was narrowest. These vibration modes should not appear if the shroud gap is uniform. Numerical simulation with non-uniform shroud gap was performed, and normal modes of a rotating disk were computed. The mode shapes of these normal modes well matched those of the measured vibration modes. Therefore, it is thought that mode amplitude at a specified point can be decreased by aerodynamic damping force.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.