LEADER 01886oam 2200541 450 001 9910707467003321 005 20160817102022.0 035 $a(CKB)5470000002464857 035 $a(OCoLC)761139430 035 $a(EXLCZ)995470000002464857 100 $a20111115j198011 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aMethod for estimating crack-extension resistance curve from residual-strength data /$fThomas W. Orange 210 1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dNovember 1980. 215 $a1 online resource (11 pages) $cillustrations 225 1 $aNASA technical paper ;$v1753 300 $aTitle from title screen (viewed on Aug. 17, 2016). 300 $a"November 1980." 320 $aIncludes bibliographical references (page 11). 606 $aCracking (fracturing)$2nasat 606 $aFailure analysis$2nasat 606 $aFracture mechanics$2nasat 606 $aFracture strength$2nasat 606 $aLoads (forces)$2nasat 606 $aFracture mechanics$2fast 615 7$aCracking (fracturing) 615 7$aFailure analysis. 615 7$aFracture mechanics. 615 7$aFracture strength. 615 7$aLoads (forces) 615 7$aFracture mechanics. 700 $aOrange$b Thomas W.$01418051 712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCQ 801 2$bOCLCO 801 2$bGPO 906 $aBOOK 912 $a9910707467003321 996 $aMethod for estimating crack-extension resistance curve from residual-strength data$93528344 997 $aUNINA LEADER 01959nam 2200457z- 450 001 9910508306603321 005 20211112 010 $a1000135139 035 $a(CKB)5590000000630144 035 $a(oapen)https://directory.doabooks.org/handle/20.500.12854/72757 035 $a(oapen)doab72757 035 $a(EXLCZ)995590000000630144 100 $a20202111d2021 |y 0 101 0 $aeng 135 $aurmn|---annan 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 00$aDynamics of Rotors on Refrigerant-Lubricated Gas Foil Bearings 210 $aKarlsruhe$cKIT Scientific Publishing$d2021 215 $a1 online resource (194 p.) 225 1 $aSchriftenreihe des Instituts für Technische Mechanik, Karlsruher Institut für Technologie 311 08$a3-7315-1112-6 330 $aThe gas foil bearing (GFB) technology is a key factor for the transition to oil-free rotating machinery. Among numerous advantages, GFBs offer the unique ability to be lubricated with working fluids such as refrigerants. However, the computational analysis of refrigerant-lubricated GFB-rotor systems represents an interdisciplinary problem of enormous complexity. This work pushes forward existing limits of feasibility and establishes a new strategy that enables stability and bifurcation analyses. 606 $aMechanical engineering & materials$2bicssc 610 $aBifurcation Analysis 610 $aBifurkationsanalyse 610 $aFluid Film Lubrication 610 $aFluidschmierung 610 $aRotor Dynamics 610 $aRotordynamik 610 $aThermodynamics 610 $aThermodynamik 610 $aTribologie 610 $aTribology 615 7$aMechanical engineering & materials 700 $aLeister$b Tim$4auth$01282227 906 $aBOOK 912 $a9910508306603321 996 $aDynamics of Rotors on Refrigerant-Lubricated Gas Foil Bearings$93018736 997 $aUNINA