Development of a Concept for Forced Response Investigations

Striving to improve performance and lower weight of aircraft engines, modern compressor blades become thinner and lighter but higher loaded resulting in an increased vulnerability towards flutter. This trend is further aggravated through blisk designs that diminish structural damping and therewith f...

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Bibliographic Details
Main Author: Holzinger, Felix
Other Authors: Mechanical Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/46074
http://scholar.lib.vt.edu/theses/available/etd-12032009-193449/