Impact and penetration of thin aluminum 2024 flat panels at oblique angles of incidence /

Bibliographic Details

Main Author:	Ruggeri, Charles R. (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2015.
Series:	NASA technical memorandum ; 2015-218484.
Subjects:	Aluminum. Finite element method. Computational mechanics. Stress distribution. Impact tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo65850