Theoretical research on dynamic modeling of rigid–flexible coupling system with double joint folded wing
For meeting the requirements of tactical missiles seeking miniaturized launch devices for storage, transportation, and launch, a tube-launched missile wing is adopted, which folds before launch and quickly unfolds after launch. As a structure installed on the missile body to generate the required ae...
| Published in: | AIP Advances |
|---|---|
| Main Authors: | , , , , , , , |
| Format: | Article |
| Language: | English |
| Published: |
AIP Publishing LLC
2024-04-01
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| Online Access: | http://dx.doi.org/10.1063/5.0186002 |
