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

Description
Item Description:	"February 2023." GPO Cataloging Record Distribution Program (CRDP).
Physical Description:	1 online resource (vi, 9 pages) : illustrations (some color).
Bibliography:	Includes bibliographical references (page 9).