Theory and Methodology of Optimally Measuring Vibratory Strains in Closely Spaced Modes

Author:

Yang M.-T.1,Griffin J. H.1

Affiliation:

1. Carnegie Mellon University, Department of Mechanical Engineering, Pittsburgh, PA 15213

Abstract

Stress ratios are traditionally used to infer maximum stresses in blades from strain measurements. This method may not be applicable to all the modes of modern low aspect ratio (LAR) blades since LAR blades often have high frequency “tip” modes that are so closely spaced that slight changes in structural properties can cause significant mode shape changes. In this paper, it is first shown that the actual tip modes of a LAR blade can be well approximated as linear combinations of the “nominal” modes. The stress field of the blade can then be estimated by calculating the modal content from multiple strain measurements. However, since placement and gage inaccuracies can introduce significant errors in the calculation, it is necessary to find the optimal gage placement that minimizes the error in estimated stresses. An error estimate using “norms” and an efficient optimization method are developed for this purpose.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference7 articles.

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2. Ben-Israel, A., and Greville, T. N. E., 1974, Generalized Inverses: Theory and Applications, Wiley, New York.

3. Kim N. , and GriffinJ. H., 1994, “Sensitivity of Bonded and Composite Beams,” Journal of Sound and Vibration, Vol. 177, pp. 71–92.

4. Meirovitch, L., 1980, Computational Methods in Structural Dynamics, Alphen aan den Rijn, The Netherlands.

5. Press, W. H., Teukolsky, S. A., Vetterling, W. T., and Flannery, B. P., 1992, Numerical Recipes in C, The Art of Scientific Computing, 2nd ed., Cambridge University Press, New York.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Robust Optimal Positioning of Strain Gages on Blades;Journal of Turbomachinery;2003-01-01

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