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Massachusetts Institute of Technology
Vibration and crack detection in gas turbine engine compressor blades using Eddy current sensors
Abstract
dc:description.abstract(cont.) in the ECS signal, no definitive method for sensing blade vibration using an ECS has yet been developed.
Degree
thesis:*- Department dc:contributor.department
- Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
- Grantor dc:publisher
- Massachusetts Institute of Technology
- Year dc:date.issued
- 2004
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Lackner, Matthew, 1980-
- Advisor dc:contributor.advisor
-
- James D. Paduano.
Subjects
dc:subject × 1Rights
dc:rights- Statement dc:rights
-
- M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
- Licence dc:rights.uri
- Language dc:language.iso
- en_US
Identifiers
dc:identifier.*- Handle dc:identifier.uri
- http://hdl.handle.net/1721.1/28895
- OAI identifier oai:identifier
- oai:dspace.mit.edu:1721.1/28895