Peer Review : Numerical Simulation of Flexible Wing of HALE UAV using Two-Way Fluid Structure Interaction Method

-, Buyung Junaidin Peer Review : Numerical Simulation of Flexible Wing of HALE UAV using Two-Way Fluid Structure Interaction Method. -. (Unpublished)

[img] Text
Peer review 1.docx

Download (629kB)
Item Type: Other
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

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year