Effect of loading rate on the open hole compression strength of quasi-isotropic carbon/epoxy laminates /

Bibliographic Details

Main Authors:	Nettles, A. T. (Alan T.) (Author), Sadowski, I. M. (Author)
Format:	Government Document eBook
Language:	English
Published:	Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, February 2023.
Series:	NASA technical memorandum ; 20230002220.
Subjects:	Composite materials. Creep rupture strength. Laminates.
Online Access:	https://purl.fdlp.gov/GPO/gpo194429