An improved single-parameter tip-timing method for turbomachinery blade vibration measurements using optical laser probes-Reference-Cited by-同舟云学术

An improved single-parameter tip-timing method for turbomachinery blade vibration measurements using optical laser probes

Published:1996-10 Issue:10 Volume:38 Page:1047-1058
ISSN:0020-7403
Container-title:International Journal of Mechanical Sciences
language:en
Short-container-title:International Journal of Mechanical Sciences

Author:

Heath S.,Imregun M.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Civil and Structural Engineering

Reference8 articles.

1. Detection and study of compressor blade vibration;Hohenberg;Exp. Mech.,1967

2. Optical detection of blade flutter;Nieberding;NASA Technical Memorandum NASA TM X-73573,1977

3. Performance evaluation of a prototype non-interference technique for measurement of turbine compressor blade stress;McCarty;Arnold Engineering Development Centre Technical Report, AEDC-TR-80-5,1980

4. Development of a non-interference technique for measuring turbine engine rotor blade stresses;Jones,1985

5. A real time non-interference stress measurement system (NSMS) for determining aero engine blade stresses;Robinson;Instrument Society of America paper #91-103,1991

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