DESIGN OF A TACTICAL UNMANNED AIR VEHICLE (TUAV) WING STRUCTURE CONCERNING STATIC, BUCKLING, AND AEROELASTIC CONSTRAINT
The significant advancements in Tactical Unmanned Aerial Vehicle (TUAV) development have prompted Indonesian Air Force's Research and Development Agency (Dislitbangau) to conduct in-depth research on TUAV for military applications. The research object chosen by Dislitbangau is a Medium Altitude...
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| 主要作者: | |
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| 格式: | Final Project |
| 語言: | Indonesia |
| 在線閱讀: | https://digilib.itb.ac.id/gdl/view/74252 |
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| 機構: | Institut Teknologi Bandung |
| 語言: | Indonesia |