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Identification of Structural Component Failures Under Dynamic Loading
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Sector:
Event:
Aerospace Meeting
Language:
English
Abstract
For purposes of parameter identification, a class of N-degree of freedom dynamical systems are decoupled, to a single degree of freedom subsystem. This is achieved by utilizing all measured accelerations, and a coordinate transformation. In cases where additional data of strains or displacements are available, the decoupled equations are further simplified. The merits of this decoupling are clearly indicated.
Citation
Simonian, S. and Hart, G., "Identification of Structural Component Failures Under Dynamic Loading," SAE Technical Paper 770958, 1977, https://doi.org/10.4271/770958.Also In
References
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