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...

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Detalles Bibliográficos
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
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Article
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

Internet

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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