Optimum Strain Gage Application to Bladed Assemblies
Author:
Affiliation:
1. Thermal Machinery Lab, ABB Turbo Systems Ltd., CH-5401 Baden, Switzerland
2. Turbomachinery Lab, Swiss Federal Institute of Technology, Zurich, Switzerland
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/124/4/606/5529366/606_1.pdf
Reference15 articles.
1. Kielb, J. J., and Abhari, R. S., 2001, “Experimental Study of Aerodynamic and Structural Damping in a Full-Scale Rotating Turbine,” ASME Paper 2001-GT-0262.
2. Purcell, T. E., May 1996, “Dynamic Stress Analysis of Gas Turbine Rotor Airfoil Using Thermoelastic Techniques,” Exp. Tech., pp. 9–13.
3. Studer, A., 1980, “Messortbestimmung fu¨r Schaufelschwingungsmessungen mit Dehnmesstreifen (Estimation of Strain Gauge Placements for Blade Vibration Measurement),” ABB Turbo Systems Ltd., Technischer Bericht HTX-ST 80024, Baden.
4. Nichol, K. L., 1991, “Strain-Gage Placement Considerations for Dynamic Data Analysis,” American Institute of Aeronautics and Astronautics, AIAA-91-1250, Tennessee.
5. Sensmeier, M. D., and Nichol, K. L., 1998, “Minimizing Vibratory Strain Measurement Error,” Proceedings of the 1998 International Gas Turbine & Aeroengine Congress & Exhibition, 98-GT-257, Stockholm.
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