Vibrations of Blades With Variable Thickness and Curvature by Shell Theory

[+] Author and Article Information
J. K. Lee, A. W. Leissa, A. J. Wang

Department of Engineering Mechanics, The Ohio State University, Columbus, Ohio 43210

J. Eng. Gas Turbines Power 106(1), 11-16 (Jan 01, 1984) (6 pages) doi:10.1115/1.3239522 History: Received December 27, 1982; Online October 15, 2009


A procedure for analyzing the vibrations of rotating turbomachinery blades has been previously developed. This procedure is based upon shallow shell theory, and utilizes the Ritz method to determine frequencies and mode shapes. However, it has been limited heretofore to blades of uniform thickness, uniform curvature, and/or twist and rectangular planform. The present work shows how the procedure may be generalized to eliminate the aforementioned restrictions. Nonrectangular planforms are dealt with by a suitable coordinate transformation. This, as well as variable thickness, curvature and twist, require using numerical integration. The procedure is demonstrated on four examples of cantilevered blades for which theoretical and experimental data have been previously published: (1) flat plate with spanwise taper, (2) flat plate with chordwise taper, (3) twisted plate with chordwise taper, and (4) cylindrical shell with chordwise taper.

Copyright © 1984 by ASME
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