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RESEARCH PAPERS: Vibrations Papers

The Effect of Stringer Width and Damping on the Response of Skin—Stringer Structures

[+] Author and Article Information
J. P. Henderson

Air Force Materials Laboratory (AFML/LLD), Wright-Patterson AFB, Ohio

A. D. Nashif

Research Institute, University of Dayton, Dayton, Ohio

J. Eng. Ind 94(1), 159-166 (Feb 01, 1972) (8 pages) doi:10.1115/1.3428105 History: Received June 11, 1971; Online July 15, 2010

Abstract

Analytical and experimental results for a five-span skin-stringer structure are presented. The analysis uses a transfer matrix technique which considers the effects of stringer dimensions including finite stringer width and damping on the computed forced response. Resonant frequencies, frequency response functions, damping and mode shapes for the first group of modes are compared for theoretical and experimental results. This agreement is found to be good.

Copyright © 1972 by ASME
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