Pages that link to "Item:Q2049751"
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The following pages link to Thermal alternation induced vibration analysis of spacecraft with lateral solar arrays in orbit (Q2049751):
Displaying 5 items.
- Dynamics of a rotating flexible and symmetric spacecraft using impedance matrix in terms of the flexible appendages cantilever modes (Q934768) (← links)
- Dynamical modeling and attitude analysis for the spacecraft with lateral solar arrays (Q2307026) (← links)
- Thermoelastic-structural dynamics analysis of a satellite with composite thin-walled boom (Q2694675) (← links)
- Thermal flutter analysis of large-scale space structures based on finite element method (Q3587757) (← links)
- Thermal-structural coupling analysis for multiple honeycomb plates connected by hinges (Q6537883) (← links)