LEADER 01442nam  2200349Ka 450 
001 9910694697403321
005 20051019083807.0
035   $a(CKB)5470000002363721
035   $a(OCoLC)62102148
035   $a(EXLCZ)995470000002363721
100   $a20051018d2005      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aMethods of analysis and failure predictions for adhesively bonded joints of uniform and variable bondline thickness$b[electronic resource] $efinal report
210  1$aWashington, D.C. :$cU.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research,$d[2005]
215   $a1 volume $cdigital, PDF file
300   $aTitle from title screen (viewed on Oct. 18, 2005).
300   $a"May 2005."
517   $aMethods of analysis and failure predictions for adhesively bonded joints of uniform and variable bondline thickness 
606   $aAdhesive joints$xTesting
606   $aTitanium$xTesting
615  0$aAdhesive joints$xTesting.
615  0$aTitanium$xTesting.
712 02$aUnited States.$bFederal Aviation Administration.$bOffice of Aviation Research.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910694697403321
996   $aMethods of analysis and failure predictions for adhesively bonded joints of uniform and variable bondline thickness$93431189
997   $aUNINA