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01438aam a22003617a 4500 001 C2F0E66E650911E6BA021E8ADAD10320 003 SILO 005 20160818010336 008 970819s1997 vau b f000 0 eng d 035 $a (OCoLC)37496094 040 $a GPO $c GPO $d DLC $d MvI $d SILO 074 $a 0830-D (MF) 086 0 $a NAS 1.15:110302 100 1 $a McGowan David M. 245 10 $a Compression response of a sandwich fuselage keel panel with and without damage $h [microform] / $c David M. McGowan and Damodar R. Ambur. 260 $a Hampton, Va. : $b National Aeronautics and Space Administration, Langley Research Center ; $c 1997] 300 $a 1 v. 440 0 $a NASA technical memorandum $v 110302 500 $a Distributed to depository libraries in microfiche. 500 $a Shipping list no.: 97-0681-M. 533 $a Microfiche. $b [Washington, D.C. : $c National Aeronautics and Space Administration, $d 1997] $e 1 microfiche. 650 7 $a Sandwich structures. $2 nasat 650 7 $a Graphite-epoxy composites . $2 nasat 650 7 $a Composite structures. $2 nasat 650 7 $a Finite element method $2 nasat 650 7 $a Fuselages. $2 nasat 650 7 $a Honeycomb cores. $2 nasat 650 7 $a Impact damage. $2 nasat 700 1 $a Ambur, Damodar R. 710 2 $a Langley Research Center 941 $a 1 952 $l USUX851 $d 20160818020351.0 956 $a http://locator.silo.lib.ia.us/search.cgi?index_0=id&term_0=C2F0E66E650911E6BA021E8ADAD10320Initiate Another SILO Locator Search