On tuned bladed disk dynamics: Some aspects of friction related mistuning-Reference-Cited by-同舟云学术

On tuned bladed disk dynamics: Some aspects of friction related mistuning

Published:1983-01 Issue:1 Volume:86 Page:107-128
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Muszyńska A.,Jones D.I.G.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference32 articles.

1. Reliability of compressor aerofoils;Passey;Progess in Aerospace Science,1976

2. Aerodynamics of compressor blade vibration;Pearson,1953

3. Blade vibration, some key elements in design verification;Danforth;Journal of Aircraft,1975

4. Control of gas turbine stator blade vibration by means of enamel coatings;Jones;American Institute of Aeronautics and Astronautics, Journal of Aircraft,1975

5. Optimization of the response of frictionally damped beam type structures with reference to gas turbine compressor blading;Williams;American Society of Mechanical Engineers Paper 73-DET-108,1973

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