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Coupling Effect of Nonlinear Stiffness of Tape Spring Hinges and Flexible Deformation of Panels during Orbit Maneuvers

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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

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