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dc.contributor.authorAlderliesten, Rene. ;en_US
dc.date.accessioned2013en_US
dc.date.accessioned2020-04-28T08:54:10Z-
dc.date.available2020-04-28T08:54:10Z-
dc.date.issued2017en_US
dc.identifier.isbn9783319562278 ;en_US
dc.identifier.isbn9783319562261 (print) ;en_US
dc.identifier.urihttp://localhost/handle/Hannan/424-
dc.descriptionPrinted edition: ; 9783319562261. ;en_US
dc.descriptionen_US
dc.descriptionen_US
dc.descriptionen_US
dc.descriptionSpringerLink (Online service) ;en_US
dc.descriptionen_US
dc.descriptionen_US
dc.description.abstractThis 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. ;en_US
dc.description.statementofresponsibilityby Rene Alderliesten.en_US
dc.description.tableofcontentsI 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. ;en_US
dc.format.extentXII, 300 p. 189 illus., 116 illus. in color. ; online resource. ;en_US
dc.publisherSpringer International Publishing :en_US
dc.publisherImprint: Springer,en_US
dc.relation.ispartofseriesSolid Mechanics and Its Applications, ; 0925-0042 ; ; 236. ;en_US
dc.relation.ispartofseriesSolid Mechanics and Its Applications, ; 0925-0042 ; ; 236. ;en_US
dc.relation.haspart9783319562278.pdfen_US
dc.subjectEngineeringen_US
dc.subjectMechanics. ;en_US
dc.subjectMechanics, Applied. ;en_US
dc.subjectAerospace engineering. ;en_US
dc.subjectAstronautics. ;en_US
dc.subjectMaterials Scienceen_US
dc.subjectEngineeringen_US
dc.subjectTheoretical and Applied Mechanics. ;en_US
dc.subjectCharacterization and Evaluation of Materials. ;en_US
dc.subjectAerospace Technology and Astronautics. ;en_US
dc.titleFatigue and Fracture of Fibre Metal Laminatesen_US
dc.typeBooken_US
dc.publisher.placeCham :en_US
dc.classification.lcTA349-359 ;en_US
dc.classification.dc620.1 ; 23 ;en_US
Appears in Collections:مهندسی مدیریت ساخت

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Full metadata record
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dc.contributor.authorAlderliesten, Rene. ;en_US
dc.date.accessioned2013en_US
dc.date.accessioned2020-04-28T08:54:10Z-
dc.date.available2020-04-28T08:54:10Z-
dc.date.issued2017en_US
dc.identifier.isbn9783319562278 ;en_US
dc.identifier.isbn9783319562261 (print) ;en_US
dc.identifier.urihttp://localhost/handle/Hannan/424-
dc.descriptionPrinted edition: ; 9783319562261. ;en_US
dc.descriptionen_US
dc.descriptionen_US
dc.descriptionen_US
dc.descriptionSpringerLink (Online service) ;en_US
dc.descriptionen_US
dc.descriptionen_US
dc.description.abstractThis 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. ;en_US
dc.description.statementofresponsibilityby Rene Alderliesten.en_US
dc.description.tableofcontentsI 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. ;en_US
dc.format.extentXII, 300 p. 189 illus., 116 illus. in color. ; online resource. ;en_US
dc.publisherSpringer International Publishing :en_US
dc.publisherImprint: Springer,en_US
dc.relation.ispartofseriesSolid Mechanics and Its Applications, ; 0925-0042 ; ; 236. ;en_US
dc.relation.ispartofseriesSolid Mechanics and Its Applications, ; 0925-0042 ; ; 236. ;en_US
dc.relation.haspart9783319562278.pdfen_US
dc.subjectEngineeringen_US
dc.subjectMechanics. ;en_US
dc.subjectMechanics, Applied. ;en_US
dc.subjectAerospace engineering. ;en_US
dc.subjectAstronautics. ;en_US
dc.subjectMaterials Scienceen_US
dc.subjectEngineeringen_US
dc.subjectTheoretical and Applied Mechanics. ;en_US
dc.subjectCharacterization and Evaluation of Materials. ;en_US
dc.subjectAerospace Technology and Astronautics. ;en_US
dc.titleFatigue and Fracture of Fibre Metal Laminatesen_US
dc.typeBooken_US
dc.publisher.placeCham :en_US
dc.classification.lcTA349-359 ;en_US
dc.classification.dc620.1 ; 23 ;en_US
Appears in Collections:مهندسی مدیریت ساخت

Files in This Item:
File Description SizeFormat 
9783319562278.pdf12.53 MBAdobe PDFThumbnail
Preview File
Full metadata record
DC FieldValueLanguage
dc.contributor.authorAlderliesten, Rene. ;en_US
dc.date.accessioned2013en_US
dc.date.accessioned2020-04-28T08:54:10Z-
dc.date.available2020-04-28T08:54:10Z-
dc.date.issued2017en_US
dc.identifier.isbn9783319562278 ;en_US
dc.identifier.isbn9783319562261 (print) ;en_US
dc.identifier.urihttp://localhost/handle/Hannan/424-
dc.descriptionPrinted edition: ; 9783319562261. ;en_US
dc.descriptionen_US
dc.descriptionen_US
dc.descriptionen_US
dc.descriptionSpringerLink (Online service) ;en_US
dc.descriptionen_US
dc.descriptionen_US
dc.description.abstractThis 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. ;en_US
dc.description.statementofresponsibilityby Rene Alderliesten.en_US
dc.description.tableofcontentsI 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. ;en_US
dc.format.extentXII, 300 p. 189 illus., 116 illus. in color. ; online resource. ;en_US
dc.publisherSpringer International Publishing :en_US
dc.publisherImprint: Springer,en_US
dc.relation.ispartofseriesSolid Mechanics and Its Applications, ; 0925-0042 ; ; 236. ;en_US
dc.relation.ispartofseriesSolid Mechanics and Its Applications, ; 0925-0042 ; ; 236. ;en_US
dc.relation.haspart9783319562278.pdfen_US
dc.subjectEngineeringen_US
dc.subjectMechanics. ;en_US
dc.subjectMechanics, Applied. ;en_US
dc.subjectAerospace engineering. ;en_US
dc.subjectAstronautics. ;en_US
dc.subjectMaterials Scienceen_US
dc.subjectEngineeringen_US
dc.subjectTheoretical and Applied Mechanics. ;en_US
dc.subjectCharacterization and Evaluation of Materials. ;en_US
dc.subjectAerospace Technology and Astronautics. ;en_US
dc.titleFatigue and Fracture of Fibre Metal Laminatesen_US
dc.typeBooken_US
dc.publisher.placeCham :en_US
dc.classification.lcTA349-359 ;en_US
dc.classification.dc620.1 ; 23 ;en_US
Appears in Collections:مهندسی مدیریت ساخت

Files in This Item:
File Description SizeFormat 
9783319562278.pdf12.53 MBAdobe PDFThumbnail
Preview File