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- W2365912138 abstract "A finite element method(FEM) was developed to analyze the stability of coupled thermal-dynamic systems of flexible appendages in spacecrafts in-orbit.The system governing equations include dynamic equations related to the transient temperature field and nonlinear transient heat conduction equations,in which radiation heat transfer is considered and structural deformations are coupled.The coupling effect and the radiation create a highly nonlinear system.The criterion for thermally-induced oscillatory stability of large space structures was established using nonlinear vibration theories.Different stability boundaries for different structures can be obtained,which divide the parametric space into stable and unstable regions.A stability analysis of the solar arrays on the Hubble Space Telescope agrees well with reference data.The effects of structural properties and heating conditions on the motion stability of a more complex antenna are also discussed based on the parameters related to thermal flutter obtained." @default.
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- W2365912138 date "2007-01-01" @default.
- W2365912138 modified "2023-09-23" @default.
- W2365912138 title "Stability analysis of coupled thermal-dynamic systems in space structures based on FEM" @default.
- W2365912138 hasPublicationYear "2007" @default.
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