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010   $a3-319-56227-4
024 7 $a10.1007/978-3-319-56227-8
035   $a(CKB)3710000001177667
035   $a(DE-He213)978-3-319-56227-8
035   $a(MiAaPQ)EBC4844351
035   $a(PPN)20051220X
035   $a(EXLCZ)993710000001177667
100   $a20170420d2017      u|         0
101 0 $aeng
135   $aurnn|008mamaa
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFatigue and Fracture of Fibre Metal Laminates /$fby René Alderliesten
205   $a1st ed. 2017.
210  1$aCham :$cSpringer International Publishing :$cImprint: Springer,$d2017.
215   $a1 online resource (XII, 300 p. 189 illus., 116 illus. in color.) 
225 1 $aSolid Mechanics and Its Applications,$x0925-0042 ;$v236
311   $a3-319-56226-6 
320   $aIncludes bibliographical references at the end of each chapters and index.
327   $aI Laminate concepts and properties -- 1 Introduction -- 2 Intellectual property and patents -- 3 Laminate concepts and typical properties -- II Prediction & analysis methods -- 1 Stress-train -- 2 Blunt notch strength -- 3 Bearing strength -- 4 Fatigue initiation -- 5 Static and fatigue delamination -- 6 Fatigue crack propagation -- 7 Residual strength -- III Environmental aspects -- 1 Temperature -- 2 Effect of frequency (wave form, hold time) -- 3 Acoustic fatigue.
330   $aThis book contributes to the field of hybrid technology, describing the current state of knowledge concerning the hybrid material concept of laminated metallic and composite sheets for primary aeronautical structural applications. It is the only book to date on fatigue and fracture of fibre metal laminates (FMLs). The first section of the book provides a general background of the FML technology, highlighting the major FML types developed and studied over the past decades in conjunction with an overview of industrial developments based on filed patents. In turn, the second section discusses the mechanical response to quasi-static loading, together with the fracture phenomena during quasi-static and cyclic loading. To consider the durability aspects related to strength justification and certification of primary aircraft structures, the third section discusses thermal aspects related to FMLs and their mechanical response to various environmental and acoustic conditions.
410  0$aSolid Mechanics and Its Applications,$x0925-0042 ;$v236
606   $aMechanics
606   $aMechanics, Applied
606   $aMaterials science
606   $aAerospace engineering
606   $aAstronautics
606   $aTheoretical and Applied Mechanics$3https://scigraph.springernature.com/ontologies/product-market-codes/T15001
606   $aCharacterization and Evaluation of Materials$3https://scigraph.springernature.com/ontologies/product-market-codes/Z17000
606   $aAerospace Technology and Astronautics$3https://scigraph.springernature.com/ontologies/product-market-codes/T17050
615  0$aMechanics.
615  0$aMechanics, Applied.
615  0$aMaterials science.
615  0$aAerospace engineering.
615  0$aAstronautics.
615 14$aTheoretical and Applied Mechanics.
615 24$aCharacterization and Evaluation of Materials.
615 24$aAerospace Technology and Astronautics.
676   $a620.1186
700   $aAlderliesten$b René$4aut$4http://id.loc.gov/vocabulary/relators/aut$0964456
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910254324903321
996   $aFatigue and Fracture of Fibre Metal Laminates$92188102
997   $aUNINA