Estimating the energy dissipated in a bolted spacecraft at resonance

Computers and Structures

Volumn 84, Issue 5-6, 2006, Pages 340-350

  Crocombe, A D ^a   Wang, R ^a   Richardson, G ^b   Underwood, C I ^a  

^a UNIVERSITY OF SURREY   (United Kingdom)

^b SURREY SATELLITE TECHNOLOGY LTD   (United Kingdom)

Author keywords

Bolted joints; Contact elements; Energy dissipation; FE model; Non linear analysis; Spacecraft structure

Indexed keywords

BOLTED JOINTS; FINITE ELEMENT METHOD; RESONANCE; SATELLITES; SPACECRAFT;

CONTACT ELEMENTS; FE MODEL; NON-LINEAR ANALYSIS; SPACECRAFT STRUCTURE;

ENERGY DISSIPATION;

EID: 29244469085     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruc.2005.09.024     Document Type: Article

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