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pro vyhledávání: '"Homero Paula Silva"'
Publikováno v:
Journal of Aerospace Technology and Management, Vol 8, Iss 3, Pp 363-372 (2016)
Carbon fiber/phenolic resin composites have long been used as ablative materials in rocketry. Ablation is a complex multiscale problem where radiative and convective heating leads to the pyrolysis of phenolic resin matrix, resulting in the formation
Externí odkaz:
https://doaj.org/article/bd93ffff9bc64eb490779bc1fc9c5033