A numerical procedure for the analysis of a vibrating panel in critical flutter conditions
Author:
Publisher
Elsevier BV
Subject
Computer Science Applications,Mechanical Engineering,General Materials Science,Modeling and Simulation,Civil and Structural Engineering
Reference11 articles.
1. Finite elements applied to panel flutter;Olson;A1AA Jnl,1967
2. Panel flutter in hypersonic flow;Bailie;AIAA Jnl,1968
3. Engineering estimates for supersonic flutter of curved shell segments;Anderson;AIAA Jnl,1970
4. Flutter analysis of thin cracked panels using the finite elements method;Chen;AIAA Jnl,1985
5. Approximate Methods of Higher Analysis;Kantorovich,1964
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1. Influence of the nonlinear aerodynamic force components on a vibrating beam, simply supported or clamped at both ends, exposed to a high supersonic airflow along its axial direction;Journal of Mechanics of Materials and Structures;2009-05-01
2. Influence of the elastic parameters of a fluttering plate on its post-critical behavior;Journal of Mechanics of Materials and Structures;2007-07-01
3. A Ritz procedure for optimisation of cylindrical shells, formed by a nearly symmetric and balanced angle-ply composite laminate, with fixed minimum frequency;Computers & Structures;2006-12
4. Polynomial series expansion for optimisation of wing plane structures in idealised critical flutter conditions;The Aeronautical Journal;2005-01
5. Influence of non-linear forces on beam behaviour in flutter conditions;Journal of Sound and Vibration;2003-10
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