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001 9910696932103321
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035   $a(CKB)5470000002383573
035   $a(OCoLC)650086411
035   $a(EXLCZ)995470000002383573
100   $a20100726d2010      uy             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSizing single cantilever beam specimens for characterizing facesheet/core peel debonding in sandwich structure /$fJames G. Ratcliffe
210  1$aHampton. Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2010]
215   $a1 online resource (36 pages) $cillustrations
225 1 $aNASA/TP-2010-216169
300   $aTitle from PDF title screen (viewed on July 26, 2010).
300   $a"January 2010.".
300   $a"Report L-19806."
320   $aIncludes bibliographical references (pages 24-26).
410  0$aNASA technical paper ;$v2010-216169.
606   $aViscoelastic materials$xTesting$xStandards
606   $aSandwich construction
615  0$aViscoelastic materials$xTesting$xStandards.
615  0$aSandwich construction.
700   $aRatcliffe$b James G$01397639
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910696932103321
996   $aSizing single cantilever beam specimens for characterizing facesheet$93469558
997   $aUNINA