LEADER 00847nam a2200241 i 4500 001 991000037879707536 005 20020509161051.0 008 950519s1990 it ||| | ita 035 $ab11299630-39ule_inst 035 $aPARLA200428$9ExL 040 $aDip.to Scienze dell'Antichità$bita 100 1 $aTurbessi, Giuseppe$0294860 245 10$aRegole monastiche antiche /$cGiuseppe Turbessi 260 $aRoma :$bStudium,$c1990 300 $a487 p. ;$c19 cm. 490 0 $aReligione e società st ;$v15. 650 4$aMonachesimo 907 $a.b11299630$b23-02-17$c01-07-02 912 $a991000037879707536 945 $aLE007 201 - 14$g1$i2015000098788$lle007$o-$pE0.00$q-$rl$s- $t0$u7$v10$w7$x0$y.i11467162$z01-07-02 996 $aRegole monastiche antiche$9866257 997 $aUNISALENTO 998 $ale007$b01-01-95$cm$da $e-$fita$git $h0$i1 LEADER 01614nam 2200409 450 001 9910716961403321 005 20211108100821.0 035 $a(CKB)5470000002526581 035 $a(OCoLC)1284802668 035 $a(EXLCZ)995470000002526581 100 $a20211108j196701 ua 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aApplication of a method of estimating high temperature low cycle fatigue behavior of materials /$fby G.R. Halford and S.S. Manson 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$d[January 1967]. 215 $a1 online resource (approximately 26 pages) $cillustrations 225 1 $aNASA/TM ;$vX-52357 300 $a"Technical paper proposed for presentation at National Metal Congress sponsored by the American Society for Metals Cleveland, Ohio, October 19, 1967." 320 $aIncludes bibliographical references (pages 8-10). 606 $aFatigue (materials)$2nasat 606 $aCreep rupture strength$2nasat 606 $aTemperature effects$2nasat 615 7$aFatigue (materials) 615 7$aCreep rupture strength. 615 7$aTemperature effects. 700 $aHalford$b Gary R.$01139998 702 $aManson$b S. S. 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910716961403321 996 $aApplication of a method of estimating high temperature low cycle fatigue behavior of materials$93512949 997 $aUNINA