The Impact Response of Carbon/Epoxy Laminates (Center Director's Discretionary Fund, Project No. 94-13) by National Aeronautics and Space Adm Nasa

The Impact Response of Carbon/Epoxy Laminates (Center Director's Discretionary Fund, Project No. 94-13)

National Aeronautics and Space Adm Nasa

180 pages • missing pub info (view editions)

nonfiction science informative medium-paced
Powered by AI (Beta)
Loading...

Description

Low velocity dropweight impact tests were conducted on carbon/epoxy laminates under various boundary conditions. The composite plates were 8-ply (+45,0, -45,90)s laminates supported in a clamped-clamped/free-free configuration with varying amounts...

Read more

Community Reviews

Loading...

Content Warnings

Loading...