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01542aam a22003857a 4500 001 C2C1611E650911E6BA021E8ADAD10320 003 SILO 005 20160818010336 008 991108s1996 dcu b f000 0 eng d 035 $a (OCoLC)42787290 040 $a GPO $c GPO $d DLC $d MvI $d SILO 074 $a 0830-D (MF) 086 0 $a NAS 1.15:111889 245 00 $a Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads $h [microform] / $c James H. Starnes, Jr. ... [et al.]. 260 $a [Washington, D.C. : $b National Aeronautics and Space Administration ; $c 1996] 300 $a 1 v. 490 1 $a NASA-TM ; $v 111889 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 Crack propagation. $2 nasat 650 7 $a Stress intensity factors. $2 nasat 650 7 $a Fuselages. $2 nasat 650 7 $a Shells (Dtructural forms) $2 nasat 650 7 $a Residual strength. $2 nasat 650 7 $a Reinforced shells. $2 nasat 650 7 $a Stress concentration $2 nasat 650 7 $a Finite element method $2 nasat 650 7 $a Structural analysis. $2 nasat 700 0 $a Starnes, James H. 710 1 $a United States. $b National Aeronautics and Space Administration 830 0 $a NASA technical memorandum $v 111889. 941 $a 2 952 $l OVUX522 $d 20180104032715.0 952 $l USUX851 $d 20160818020347.0 956 $a http://locator.silo.lib.ia.us/search.cgi?index_0=id&term_0=C2C1611E650911E6BA021E8ADAD10320Initiate Another SILO Locator Search