Effect of Stiffener Geometry on the Response of Grid-Stiffened Panels
Publication: Journal of Engineering Mechanics
Volume 144, Issue 2
Abstract
It is well established that the lateral bending stiffness of thin panels is considerably enhanced by judicious use of ribs or stiffeners. This increase in stiffness is primarily due to a disproportionate increase in the second moment of area, and because relatively little mass is added, stiffened panels are especially appealing in an aerospace engineering context. In experiments it is relatively straightforward to measure bending deflections (especially in a cantilever configuration) and natural frequencies using laser vibrometry and associated signal-processing tools. This paper reports on a parametric study in which bending stiffness and natural frequencies are measured for a set of rectangular panels, conveniently manufactured using a three-dimensional (3D) printer. Both isogrid (stiffeners in a triangular configuration) and orthogrid (stiffeners in a rectangular configuration) structures were made and tested, with certain nondimensional parameters held constant (for example, total mass and length-to-width ratio) to facilitate easier comparison. The boundary condition considered was one edge clamped and the other edges free (simple cantilever) with a consistent plan area aspect ratio, and with the height and arrangement of stiffening ribs providing the major parametric variation.
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Acknowledgments
Financial support for this project was provided by the Air Force Office of Scientific Research under Award No. FA9550-13-1-0130. This support is greatly appreciated. Data acquisition was assisted by Duke undergraduates William Shelburne, Eric Essoyan, and Nick Danyluk.
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©2017 American Society of Civil Engineers.
History
Received: May 24, 2017
Accepted: Aug 25, 2017
Published online: Dec 14, 2017
Published in print: Feb 1, 2018
Discussion open until: May 14, 2018
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