LEADER 02095oam  2200601I  450 
001 9910713886603321
005 20200824104113.0
035   $a(CKB)5470000002504824
035   $a(OCoLC)1100474456
035   $a(EXLCZ)995470000002504824
100   $a20190508d1954      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAdditional static and fatigue tests of high-strength aluminum-alloy bolted joints /$fby E.C. Hartmann, Marshall Holt, and I.D. Eaton
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1954.
215   $a1 online resource (42 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3269
300   $a"July 1954."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 14).
606   $aAluminum alloys$xFatigue
606   $aBolted joints$xTesting
606   $aJoints (Engineering)
606   $aStrength of materials
606   $aAluminum alloys$xFatigue$2fast
606   $aBolted joints$xTesting$2fast
606   $aJoints (Engineering)$2fast
606   $aStrength of materials$2fast
615  0$aAluminum alloys$xFatigue.
615  0$aBolted joints$xTesting.
615  0$aJoints (Engineering)
615  0$aStrength of materials.
615  7$aAluminum alloys$xFatigue.
615  7$aBolted joints$xTesting.
615  7$aJoints (Engineering)
615  7$aStrength of materials.
700   $aHartmann$b E. C.$01415621
702   $aHolt$b M$g(Marshall),
702   $aEaton$b I. D.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bCOP
801  2$bTRAAL
801  2$bGPO
906   $aBOOK
912   $a9910713886603321
996   $aAdditional static and fatigue tests of high-strength aluminum-alloy bolted joints$93527532
997   $aUNINA