AEROFRACTURE ANALYSIS ON UNIDIRECTIONAL COMPOSITE PLATE BY MEANS OF FINITE ELEMENT METHOD AND DOUBLET LATTICE METHOD
In the recent decades, composite materials have become key element to construct advanced structure, i.e., aircraft structure. The present work is aimed to provide insight on how fiber orientation and crack existence in dynamic characteristics and aeroelastic instability. A plate-like wing made of un...
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| Main Author: | |
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| Format: | Theses |
| Language: | Indonesia |
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| Online Access: | https://digilib.itb.ac.id/gdl/view/84459 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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