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Coupling Effect of Nonlinear Stiffness of Tape Spring Hinges and Flexible Deformation of Panels during Orbit Maneuvers
Affiliation of Author(s):机械工程学院
Journal:Aerospace
First Author:顾文艳
Document Code:C7A6816AB80A407896D6FBBB5225D671
Volume:9
Issue:1
Number of Words:6
Translation or Not:no
Date of Publication:2022-01-10