Resonant blade response in turbine rotor spin tests using a laser-light probe non-intrusive measurement system

Approved for public release; distribution is unlimited. === Procedures to qualify turbo-machinery components for a designed lifetime free of high cycle fatigue (HCF) failures have not yet evolved. As part of an initiative to address this issue, in the present study, laser-light probes were used in a...

Full description

Bibliographic Details
Main Author: Mansisidor, Michael R.
Other Authors: Shreeve, Raymond P.
Published: Monterey, California. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/5982