Devulcanized Rubber Based Composite Design Reinforced with Nano Silica, Graphene Nano Platelets (GnPs) and Epoxy for “Aircraft Wing Spar” to Withstand Bending Moment
Crossref DOI link: https://doi.org/10.1007/978-3-319-95510-0_2
Published Print: 2025-08-07
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Irez, A. B.
Bayraktar, E.
Miskioglu, I.
Text and Data Mining valid from 2025-08-07
