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035   $a(CKB)5470000002529237
035   $a(OCoLC)1158388770
035   $a(EXLCZ)995470000002529237
100   $a20200615d1941      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of alternately high and low repeated stresses upon the fatigue strength of 25ST aluminum alloy /$fby G.W. Stickley
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1941.
215   $a1 online resource (5 pages, 1 unnumbered page) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 792
300   $a"January 1941."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical reference (page 4).
606   $aAluminum alloys
606   $aAlloys$xFatigue$xTesting
606   $aStrains and stresses
606   $aAlloys$xFatigue$xTesting$2fast
606   $aAluminum alloys$2fast
606   $aStrains and stresses$2fast
615  0$aAluminum alloys.
615  0$aAlloys$xFatigue$xTesting.
615  0$aStrains and stresses.
615  7$aAlloys$xFatigue$xTesting.
615  7$aAluminum alloys.
615  7$aStrains and stresses.
700   $aStickley$b G. W.$01420364
712 02$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   $a9910717298403321
996   $aEffect of alternately high and low repeated stresses upon the fatigue strength of 25ST aluminum alloy$93537977
997   $aUNINA