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035   $a(EXLCZ)995470000002529715
100   $a20200615d1941      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of methods of testing on the ultimate loads supported by stiffened flat sheet panels under edge compression /$fby Marshall Holt
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1941.
215   $a1 online resource (19 pages, 7 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 811
300   $a"June 1941."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical reference (page 13).
606   $aAluminum alloys
606   $aSheet-metal$xTesting
606   $aMaterials$xCompression testing
606   $aLoads (Mechanics)
606   $aAluminum alloys$2fast
606   $aLoads (Mechanics)$2fast
606   $aMaterials$xCompression testing$2fast
606   $aSheet-metal$xTesting$2fast
615  0$aAluminum alloys.
615  0$aSheet-metal$xTesting.
615  0$aMaterials$xCompression testing.
615  0$aLoads (Mechanics)
615  7$aAluminum alloys.
615  7$aLoads (Mechanics)
615  7$aMaterials$xCompression testing.
615  7$aSheet-metal$xTesting.
700   $aHolt$b M$g(Marshall),$01395606
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910717251103321
996   $aThe effect of methods of testing on the ultimate loads supported by stiffened flat sheet panels under edge compression$93459740
997   $aUNINA