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01673aam a2200373Ka 4500 001 1F7A4F8069C711E69620BACFDAD10320 003 SILO 005 20160824014144 008 080616s1984 vau b f000 0 eng d 035 $a (OCoLC)232108730 040 $a GPO $c GPO $d MvI $d SILO 074 $a 0830-D (MF) 074 $a 0830-D (online) 086 0 $a NAS 1.15:85756 100 1 $a Williams, Jerry G. 245 10 $a Effect of impact damage and open holes on the compression strength of tough resin/high strain fiber laminates $h [microform] / $c Jerry G. Williams. 260 $a Hampton, Va. : $b National Aeronautics and Space Administration, Langley Research Center, $c [1984] 300 $a 1 v. 440 0 $a NASA technical memorandum $v 85756 530 $a Also available via Internet from the NTRS web site. Address as of 06/13/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19840012582%5F1984012582.pdf ; current access is available via PURL. 533 $a Microfiche. $b [Washington, D.C. : $c National Aeronautics and Space Administration], $d 1984. $e 1 microfiche. 650 0 $a Airplanes $x Design and construction 650 0 $a Composite materials $x Delamination 650 0 $a Composite materials $x Compression testing. 650 7 $a Compressive strength. $2 nasat 650 7 $a Graphite-epoxy composites . $2 nasat 650 7 $a Impact damages. $2 nasat 650 7 $a Impact tolerances. $2 nasat 650 7 $a Openings. $2 nasat 710 2 $a Langley Research Center 856 41 $u http://purl.access.gpo.gov/GPO/LPS95394 941 $a 1 952 $l USUX851 $d 20160824061022.0 956 $a http://locator.silo.lib.ia.us/search.cgi?index_0=id&term_0=1F7A4F8069C711E69620BACFDAD10320Initiate Another SILO Locator Search