NASA NTRS · 19880004253
Shape optimization of damping layers
Abstract
Shape optimization of unconstrained and constrained damping layers is completed. The specific problem analyzed is a cantilever beam loaded at its tip by a harmonic force. Finite element modeling and mathematical programming techniques are used to obtain the solution. Performance measures are taken to be reduction of maximum diplacement and increase in fatigue lifetime. Results include the improvement, over the uniform treatment case, of these measures when the profile of the damping layer is optimized.
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Lin, T.-C., Scott, R. A.. 1987-10-01. Shape optimization of damping layers. https://ntrs.nasa.gov/citations/19880004253
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