PENGUJIAN DAN ANALISIS PADA KOMPOSIT KARBON/EPOXY UD DAN FABRIC YANG DIBUAT DALAM BEBERAPA KONFIGURASI LAPISAN AKIBAT IMPACT KECEPATAN RENDAH
Laminate as structure or component on the aircraft is very risky for the impact caused by the mechanism of mechanical loading during maintenance and flight. The important things in the use of Carbon Fiber Reinforced Composite on aircraft structures is the occurrence of Low Velocity Impact (LVI) load...
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| Format: | Theses |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/33437 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |