-, Buyung Junaidin Peer Review : Numerical Simulation of Flexible Wing of HALE UAV using Two-Way Fluid Structure Interaction Method. -. (Unpublished)
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Peer review 1.docx Download (629kB) |
| Item Type: | Other |
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| Subjects: | T Technology > TL Motor vehicles. Aeronautics. Astronautics |
| Depositing User: | Mr Buyung Junaidin |
| Date Deposited: | 05 Feb 2020 05:01 |
| Last Modified: | 05 Feb 2020 05:01 |
| URI: | http://eprints.stta.ac.id/id/eprint/123 |
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