NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
An Approximate Dissipation Function for Large Strain Rubber Thermo-Mechanical AnalysesMechanically induced viscoelastic dissipation is difficult to compute. When the constitutive model is defined by history integrals, the formula for dissipation is a double convolution integral. Since double convolution integrals are difficult to approximate, coupled thermo-mechanical analyses of highly viscous rubber-like materials cannot be made with most commercial finite element software. In this study, we present a method to approximate the dissipation for history integral constitutive models that represent Maxwell-like materials without approximating the double convolution integral. The method requires that the total stress can be separated into elastic and viscous components, and that the relaxation form of the constitutive law is defined with a Prony series. Numerical data is provided to demonstrate the limitations of this approximate method for determining dissipation. Rubber cylinders with imbedded steel disks and with an imbedded steel ball are dynamically loaded, and the nonuniform heating within the cylinders is computed.
Document ID
20030067936
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Johnson, Arthur R.
(Army Research Lab. Hampton, VA, United States)
Chen, Tzi-Kang
(Army Research Lab. Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2003
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TM-2003-212430
L-18308
NAS 1.15:212430
ARL-TR-2998
Report Number: NASA/TM-2003-212430
Report Number: L-18308
Report Number: NAS 1.15:212430
Report Number: ARL-TR-2998
Funding Number(s)
PROJECT: RTOP 755-06-00-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available