A study of the damping linearity of jointed metal plates
A study of the damping linearity of jointed metal plates
Dynamic models are widely used in many branches of science and engineering and it has been argued that many of the shortfalls with these models are due to the fact that the physics of joint dynamics are not fully understood. This makes the phenomenon very hard to model theoretically from first principles. Experimental analyses are therefore widely used to underpin any work in this area. This study aims to build on the previous experimental work based on simple beam joints and analyses the damping trends for metal panels. This incorporates torsional effects into the system creating more complex displacements of the joint. Five panel configurations are investigated using an experimental approach that minimizes all external influences on the dynamics of the panels. Each mode loss factor is determined from these experimental tests and compared to the most established theoretical model in the field. The corresponding joint displacements and decay trends are also analysed, producing indications as to the likely dominant source of damping, suggesting that the mode shapes can be categorized based on their displacement and dominant damping source.
damping metal plates non-linear
1738-1746
Walker, Scott J.I.
f28a342f-9755-48fd-94ea-09e44ac4dbf5
Aglietti, Guglielmo S.
e44d0dd4-0f71-4399-93d2-b802365cfb9e
Cunningham, Paul
ddb5752a-1b1f-4832-9ca5-d45f31682258
July 2008
Walker, Scott J.I.
f28a342f-9755-48fd-94ea-09e44ac4dbf5
Aglietti, Guglielmo S.
e44d0dd4-0f71-4399-93d2-b802365cfb9e
Cunningham, Paul
ddb5752a-1b1f-4832-9ca5-d45f31682258
Walker, Scott J.I., Aglietti, Guglielmo S. and Cunningham, Paul
(2008)
A study of the damping linearity of jointed metal plates.
AIAA Journal, 46 (7), .
(doi:10.2514/1.34323).
Abstract
Dynamic models are widely used in many branches of science and engineering and it has been argued that many of the shortfalls with these models are due to the fact that the physics of joint dynamics are not fully understood. This makes the phenomenon very hard to model theoretically from first principles. Experimental analyses are therefore widely used to underpin any work in this area. This study aims to build on the previous experimental work based on simple beam joints and analyses the damping trends for metal panels. This incorporates torsional effects into the system creating more complex displacements of the joint. Five panel configurations are investigated using an experimental approach that minimizes all external influences on the dynamics of the panels. Each mode loss factor is determined from these experimental tests and compared to the most established theoretical model in the field. The corresponding joint displacements and decay trends are also analysed, producing indications as to the likely dominant source of damping, suggesting that the mode shapes can be categorized based on their displacement and dominant damping source.
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More information
Published date: July 2008
Keywords:
damping metal plates non-linear
Organisations:
Aerodynamics & Flight Mechanics, Dynamics Group, Astronautics Group
Identifiers
Local EPrints ID: 58242
URI: http://eprints.soton.ac.uk/id/eprint/58242
ISSN: 0001-1452
PURE UUID: 4b97decc-768a-4e65-8a71-45862fe844f5
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Date deposited: 18 Aug 2008
Last modified: 15 Mar 2024 11:10
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Contributors
Author:
Scott J.I. Walker
Author:
Guglielmo S. Aglietti
Author:
Paul Cunningham
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