LEADER 01655oam  2200445I  450 
001 9910706861103321
005 20180227144422.0
035   $a(CKB)5470000002458856
035   $a(OCoLC)1024083482
035   $a(OCoLC)995470000002458856
035   $a(EXLCZ)995470000002458856
100   $a20180223j194701    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of rivet or bolt holes on the ultimate strength developed by 24S-T and alclad 75S-T sheet in incomplete diagonal tension /$fby L. Ross Levin and David H. Nelson
210  1$aWashington :$cNational Advisory Committee for Aeronautics,$dJanuary 1947.
215   $a1 online resource (10 pages, 6 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 1177
300   $a"January 1947."
300   $aDistribution made by issuing office.
320   $aIncludes bibliographical references (page 9).
606   $aRivets$2nasat
606   $aAluminum alloys$2nasat
606   $aAeronautics$2nasat
615  7$aRivets.
615  7$aAluminum alloys.
615  7$aAeronautics.
700   $aLevin$b L. Ross$01420497
702   $aNelson$b David H.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910706861103321
996   $aEffect of rivet or bolt holes on the ultimate strength developed by 24S-T and alclad 75S-T sheet in incomplete diagonal tension$93538476
997   $aUNINA