Implementation of a two probe tip-timing technique to determine compressor blade vibrations
by Nicholas Glen Osburn
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This study involved the implementation and validation of a blade-tip time of arrival (TOA) measurement technique, and the development of a computer program to analyze TOA data using a recently published approach. The program was used to analyze experimental compressor data taken in-house using two laser light probes, data generated computation ally, and data obtained by others in a compressor test. The in-house compressor data was compared successfully to amplitudes obtained by strobed digital photography. A resonance was successfully detected in the supplied compressor data set.
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Implementation of a two probe tip-timing technique to determine compressor blade vibrations
2000, Naval Postgraduate School, Available from National Technical Information Service
Electronic resource
in English
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Book Details
Published in
Monterey, Calif, Springfield, Va
Edition Notes
Thesis advisors: Shreeve, Raymond P.
"June 2000."
Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, June 2000.
Includes bibliographical references (p. 41).
Approved for public release, distribution unlimited.
Also available online.
System requirements: Adobe Acrobat reader.
Mode of access: World Wide Web.
US Navy (USN) author.
dk/dk cc:9116 9/14/00
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