Descripción del título
This 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
Monografía
monografia Rebiun18767821 https://catalogo.rebiun.org/rebiun/record/Rebiun18767821 cr c 170420s2017 gw o 001 0 eng d 9783319562278 978-3-319-56227-8 10.1007/978-3-319-56227-8 doi UEM 95853 UR0416227 CBUC 991049395199706706 UPVA 996889404403706 UAM 991007839713104211 UCAR 991007886364804213 CBUC 991004932016706711 UAL spa UAL rdc 620.1 23 Alderliesten, René Fatigue and Fracture of Fibre Metal Laminates by René Alderliesten Cham Springer International Publishing Imprint: Springer 2017 Cham Cham Springer International Publishing Imprint: Springer 1 recurso en línea 1 recurso en línea XII, 300 p. 189 illus., 116 illus. in color XII, 300 p. 189 illus., 116 illus. in color Texto (visual) isbdcontent electrónico isbdmedia Springer eBooks Solid Mechanics and Its Applications 0925-0042 236 This 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 Modo de acceso: World Wide Web Engineering Mechanics Mechanics, Applied Aerospace engineering Astronautics Materials science Engineering Theoretical and Applied Mechanics Characterization and Evaluation of Materials Aerospace Technology and Astronautics Ingeniería Libros electrónicos Recursos electrónicos SpringerLink (Online service)