LEADER 02818oam  2200493   450 
001 9910299710203321
005 20190911112726.0
010   $a3-7091-1768-2
024 7 $a10.1007/978-3-7091-1768-2
035   $a(OCoLC)871041878
035   $a(MiFhGG)GVRL6WDW
035   $a(EXLCZ)993710000000078914
100   $a20140429d2014      uy             0
101 0 $aeng
135   $aurun|---uuuua
181   $ctxt
182   $cc
183   $acr
200 00$aConstitutive relations under impact loadings $eexperiments, theoretical and numerical aspects /$fTomasz Lodygowski, Alexis Rusinek, editors
205   $a1st ed. 2014.
210  1$aWien [Vienna] :$cSpringer,$d2014.
215   $a1 online resource (285 pages) $cillustrations (some color)
225 1 $aCISM International Centre for Mechanical Sciences, Courses and Lectures,$x0254-1971 ;$v552
300   $a"ISSN: 0254-1971."
311   $a3-7091-1767-4 
320   $aIncludes bibliographical references at the end of each chapters.
327   $aTesting with bars from dynamic to quasi-static -- Dynamic testing of materials -- Material behavior under dynamics loading, modeling and experiments -- Analysis of some high-speed impact problems in the aircraft industry -- Computer estimation of plastic strain localization and failure for large strain rates using viscoplasticity -- Inelastic flow and failure of metallic solids accounting for asymmetry of elastic range and micro-shear banding.
330   $aThe book describes behavior of materials (ductile, brittle and composites) under impact loadings and high strain rates. The three aspects: experimental, theoretical and numerical are in the focus of interest. Hopkinson bars are mainly used as experimental devices to describe dynamic behavior of materials. The precise description of experimental techniques and interpretation of wave interaction are carefully discussed. Theoretical background refers to rate dependent thermoviscoplastic formulation. This includes the discussion of well posedness of initial boundary value problems and the solution of the system of governing equations using numerical methods. Explicit time integration is used in computations to solve dynamic problems. In addition, many applications in aeronautic and automotive industries are exposed.
410  0$aCourses and lectures ;$vvol. 552.
606   $aMaterials$xMechanical properties
606   $aImpact
615  0$aMaterials$xMechanical properties.
615  0$aImpact.
676   $a515
676   $a515/.35
676   $a620.1125
702   $aLodygowski$b Tomasz
702   $aRusinek$b Alexis
801  0$bMiFhGG
801  1$bMiFhGG
906   $aBOOK
912   $a9910299710203321
996   $aConstitutive Relations under Impact Loadings$92105773
997   $aUNINA