ANALISIS DAN OPTIMASI STRUKTUR ANISOGRID KOMPOSIT SAYAP PESAWAT TEMPUR DENGAN KRITERIA KEGAGALAN STATIK, BUCKLING DAN FLUTTER MENGGUNAKAN METODE ELEMEN HINGGA
In this undergraduate thesis, an analysis and optimization is carried out on a fighter wing model with a composite anisogrid configuration. The analysis was conducted to determine the response of the anisogrid sandwich structure to static load, buckling, and flutter. Anisogrid structure means the st...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/61782 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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