On the Stability of the Equilibrium of Nonconservative Continuous Systems With Slight DampingSource: Journal of Applied Mechanics:;1967:;volume( 034 ):;issue: 002::page 344Author:S. Nemat-Nasser
DOI: 10.1115/1.3607688Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The stability of the equilibrium configuration of a linearly elastic solid (with or without internal damping) subjected to partial follower surface tractions (nonconservative loading) is studied. Proportional loading is considered and it is proved that the flutter (oscillations with increasing amplitude) load parameter of the undamped system is an upper bound for that of the system with slight damping. The necessary and sufficient condition for stability of the equilibrium state with respect to flutter-type motions, and sufficiency conditions for stability with respect to both divergence (or buckling) and flutter, are established. Based on energy considerations, an approximate method of stability analysis is suggested which reduces to the usual energy criterion for the cases of conservative loading.
keyword(s): Stability , Equilibrium (Physics) , Damping , Flutter (Aerodynamics) , Motion , Stress , Buckling AND Oscillations ,
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contributor author | S. Nemat-Nasser | |
date accessioned | 2017-05-08T23:49:48Z | |
date available | 2017-05-08T23:49:48Z | |
date copyright | June, 1967 | |
date issued | 1967 | |
identifier issn | 0021-8936 | |
identifier other | JAMCAV-25850#344_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/116767 | |
description abstract | The stability of the equilibrium configuration of a linearly elastic solid (with or without internal damping) subjected to partial follower surface tractions (nonconservative loading) is studied. Proportional loading is considered and it is proved that the flutter (oscillations with increasing amplitude) load parameter of the undamped system is an upper bound for that of the system with slight damping. The necessary and sufficient condition for stability of the equilibrium state with respect to flutter-type motions, and sufficiency conditions for stability with respect to both divergence (or buckling) and flutter, are established. Based on energy considerations, an approximate method of stability analysis is suggested which reduces to the usual energy criterion for the cases of conservative loading. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | On the Stability of the Equilibrium of Nonconservative Continuous Systems With Slight Damping | |
type | Journal Paper | |
journal volume | 34 | |
journal issue | 2 | |
journal title | Journal of Applied Mechanics | |
identifier doi | 10.1115/1.3607688 | |
journal fristpage | 344 | |
journal lastpage | 348 | |
identifier eissn | 1528-9036 | |
keywords | Stability | |
keywords | Equilibrium (Physics) | |
keywords | Damping | |
keywords | Flutter (Aerodynamics) | |
keywords | Motion | |
keywords | Stress | |
keywords | Buckling AND Oscillations | |
tree | Journal of Applied Mechanics:;1967:;volume( 034 ):;issue: 002 | |
contenttype | Fulltext |