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 Online: 2018-10-16
Published Print: 2019
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Irez, A. B.
Bayraktar, E.
Miskioglu, I.
Text and Data Mining valid from 2018-10-16