Fabrication and characterization of BMI specimens by DMA tests
Composite materials have begun to gain recognition in the aviation industry due to their excellent strength to weight ratio. Bismaleimides composites are slowly replacing epoxy composites. This study will provide a framework for fabricating test specimens samples by detailing procedures and equipmen...
Saved in:
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Final Year Project |
| Language: | English |
| Published: |
2014
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/60939 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Institution: | Nanyang Technological University |
| Language: | English |
| Summary: | Composite materials have begun to gain recognition in the aviation industry due to their excellent strength to weight ratio. Bismaleimides composites are slowly replacing epoxy composites. This study will provide a framework for fabricating test specimens samples by detailing procedures and equipment required. The material used for this test is 4,4’-bismaleimidodiphenylmethane combined with o,o’-diallylbisphenol A which is a common bismaleimide resin currently available in the market.
A differential scanning calorimetry test is conducted to determine the melting point before fabrication can begin. Subsequently, the samples fabricated undergo a dynamic analysis test to determine their dynamic mechanical properties. A correlation is found between the frequency tested and the properties obtained. The time-temperature superposition model is used to predict the long term behaviour of the samples.
This project has provided a detailed fabrication process and characterized the material’s dynamic properties. With the results obtained, this study will be able to contribute to existing studies on bismaleimide composites and provide a benchmark for future research. |
|---|