Material combinations and parametric study of thermal and mechanical performance of pyramidal core sandwich panels used for hypersonic aircrafts
Crossref DOI link: https://doi.org/10.1007/s00161-016-0518-x
Published Online: 2016-07-12
Published Print: 2016-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zhang, Ruiping
Zhang, Xiaoqing
Lorenzini, Giulio
Xie, Gongnan
License valid from 2016-07-12