Rigid-flexible-thermal coupling dynamic formulation for satellite and plate multibody system
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference18 articles.
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3. Thermally induced dynamics of satellite solar panels;Johnston;J. Spacecr. Rockets,2000
4. Nonlinear transient response of thermally loaded laminated panels;Oguamanam;J. Appl. Mech.,2004
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