01278cam0-22004691i-450 99000859448040332120191016155558.0000859448FED01000859448(Aleph)000859448FED0100085944820071212d2007----km-y1itaa50------baitaIT--------001cyLezioni di inferenza statisticaLuigi D'Ambra4. edNapoliRCE2007431 p.30 cmDipartimento di matematica e statistica. Università "Federico II" NapoliSerie didatticaSegue appendiceInferenza statistica519.5519.52519.5421itaD'Ambra,Luigi367573ITUNINARICAUNIMARCBK990008594480403321IX-A-11810550MAS123-I-823148MA1A / DAM 24515BFSMSSTAT64A19444DECBCMSSTAT64B19445DECBCMDSTAT64C19446DECBCMASDECBCMA1BFS62-XXLezioni di inferenza statistica438004UNINA01963nam 2200577 450 991070580880332120170814081935.0(CKB)5470000002454333(OCoLC)1000486089(EXLCZ)99547000000245433320170814j199811 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFlow/damage surfaces for fiber-reinforced metals having different periodic microstructures /Cliff J. Lissenden, Steven M. Arnold, Saiganesh K. IyerCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,November 1998.1 online resource (28 pages) illustrationsNASA/TM ;1998-208805"November 1998.""Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.Includes bibliographical references (pages 14-15).Fiber compositesnasatMetal matrix compositesnasatMicromechanicsnasatFinite element methodnasatMicrostructurenasatDamagenasatShear stressnasatStrain ratenasatTransverse loadsnasatFiber composites.Metal matrix composites.Micromechanics.Finite element method.Microstructure.Damage.Shear stress.Strain rate.Transverse loads.Lissenden Cliff Jesse1398770Arnold S. M.Iyer Saiganesh K.Lewis Research Center,GPOGPOBOOK9910705808803321Flow3462717UNINA