LEADER 00899nam a2200253 i 4500 001 991003380109707536 008 170607s2009 it 000 0 ita d 020 $a9788895724799 035 $ab14325019-39ule_inst 040 $aDip. di Studi Umanistici$bita 041 1 $aita$heng 082 0 $a813.6 100 1 $aHarris, Charlaine$0742119 245 10$aDecisamente morto :$bil sesto romanzo del ciclo di Sookie Stackhouse /$cCharlaine Harris 264 1$aMilano :$bDelos Books,$c2009 300 $a339 p. ;$c20 cm 490 0 $aOdissea.$aVampiri ;$v14 765 0 $tDefinitely dead 907 $a.b14325019$b07-06-17$c07-06-17 912 $a991003380109707536 945 $aLE012 813.6 HAR 2$g1$i2007000280652$lle012$og$pE15.90$q-$rl$s- $t0$u0$v0$w0$x0$y.i15809894$z07-06-17 996 $aDecisamente morto$91474085 997 $aUNISALENTO 998 $ale012$b07-06-17$cm$da $e-$fita$git $h0$i0 LEADER 01847oam 2200517 450 001 9910717298403321 005 20220225123329.0 035 $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