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Manufacturing ZrB(2)–SiC–TaC Composite: Potential Application for Aircraft Wing Assessed by Frequency Analysis through Finite Element Model
This study presents a new ultra-high temperature composite fabricated by using zirconium diboride (ZrB(2)), silicon carbide (SiC), and tantalum carbide (TaC) with the volume ratios of 70%, 20%, and 10%, respectively. To attain this novel composite, an advanced processing technique of spark plasma si...
Autores principales: | Mohammadzadeh, Behzad, Jung, Sunghoon, Lee, Tae Hyung, Le, Quyet Van, Cha, Joo Hwan, Jang, Ho Won, Lee, Sea-Hoon, Kang, Junsuk, Shokouhimehr, Mohammadreza |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
MDPI
2020
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7288086/ https://www.ncbi.nlm.nih.gov/pubmed/32408511 http://dx.doi.org/10.3390/ma13102213 |
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