Bridge Flutter Derivatives at Vortex Lock-InSource: Journal of Structural Engineering:;1998:;Volume ( 124 ):;issue: 004Author:Robert H. Scanlan
DOI: 10.1061/(ASCE)0733-9445(1998)124:4(450)Publisher: American Society of Civil Engineers
Abstract: Many structures with extended spans undergo the flow-induced oscillation commonly called vortex shedding. In the case of long-span bridges, Ehsan and Scanlan, employing basic data from deck section wind tunnel model tests, offered a nonlinear theoretical framework for predicting maximum vortex-induced amplitude under the lock-in condition. The present paper replaces the Ehsan-Scanlan model with a linearized form that brings it into conformity with the familiar flutter derivative expressions now commonly used in bridge wind-stability analyses. The essential new addition is an active sinusoidal lift term. Converting some of the Ehsan-Scanlan experimental section data to the new form, the suggested replacement model successfully reidentifies the range of original Tacoma Narrows vortex-induced response amplitudes that were experimentally obtained by Farquharson on a full-bridge model. Either vertical or torsional motions at vortex lock-in can be assayed by the method discussed.
|
Collections
Show full item record
contributor author | Robert H. Scanlan | |
date accessioned | 2017-05-08T20:57:04Z | |
date available | 2017-05-08T20:57:04Z | |
date copyright | April 1998 | |
date issued | 1998 | |
identifier other | %28asce%290733-9445%281998%29124%3A4%28450%29.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/32956 | |
description abstract | Many structures with extended spans undergo the flow-induced oscillation commonly called vortex shedding. In the case of long-span bridges, Ehsan and Scanlan, employing basic data from deck section wind tunnel model tests, offered a nonlinear theoretical framework for predicting maximum vortex-induced amplitude under the lock-in condition. The present paper replaces the Ehsan-Scanlan model with a linearized form that brings it into conformity with the familiar flutter derivative expressions now commonly used in bridge wind-stability analyses. The essential new addition is an active sinusoidal lift term. Converting some of the Ehsan-Scanlan experimental section data to the new form, the suggested replacement model successfully reidentifies the range of original Tacoma Narrows vortex-induced response amplitudes that were experimentally obtained by Farquharson on a full-bridge model. Either vertical or torsional motions at vortex lock-in can be assayed by the method discussed. | |
publisher | American Society of Civil Engineers | |
title | Bridge Flutter Derivatives at Vortex Lock-In | |
type | Journal Paper | |
journal volume | 124 | |
journal issue | 4 | |
journal title | Journal of Structural Engineering | |
identifier doi | 10.1061/(ASCE)0733-9445(1998)124:4(450) | |
tree | Journal of Structural Engineering:;1998:;Volume ( 124 ):;issue: 004 | |
contenttype | Fulltext |