01614nam 2200457I 450 991070438170332120160315142714.0(CKB)5470000002439865(OCoLC)944527336(EXLCZ)99547000000243986520160315j201504 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierImpact and penetration of thin aluminum 2024 flat panels at oblique angles of incidence /Charles R. Ruggeri [and four others]Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,April 2015.1 online resource (99 pages) color illustrationsNASA/TM ;2015-218484Title from title screen (viewed on March 15, 2016)."April 2015."Includes bibliographical references (page 99).AluminumnasatFinite element methodnasatComputational mechanicsnasatStress distributionnasatImpact testsnasatAluminum.Finite element method.Computational mechanics.Stress distribution.Impact tests.Ruggeri Charles R.1406007NASA Glenn Research Center,GPOGPOBOOK9910704381703321Impact and penetration of thin aluminum 2024 flat panels at oblique angles of incidence3483759UNINA