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001			95853
003			ES-MaUEC
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007			cr cnu|||unuuu
008			170424s2017 sz a ob 001 0 eng d
020			_a3319562274 _q(electronic bk.)
020			_a9783319562278 _q(electronic bk.)
020			_z3319562266
020			_z9783319562261 _q(print)
040			_aN$T _cN$T _dGW5XE _dN$T _dYDX _dEBLCP _dUAB _dESU _dAZU _dUPM _dOCLCF _dCOO _dOTZ _dOCLCQ _dIOG _dU3W _dES-MaUEC _bspa
050		4	_aTA481.5 _bA434 2017 EB
100	1		_aAlderliesten, René, _eautor
245	1	0	_aFatigue and fracture of fibre metal laminates _cRené Alderliesten.
264		1	_aCham, Switzerland _bSpringer _c2017.
300			_a1 recurso en línea (xii, 300 páginas) _bilustraciones (algunas a color)
336			_aTexto _btxt _2rdacontent
337			_aelectrónico _bc _2rdamedia
338			_arecurso electrónico _bcr _2rdacarrier
347			_atext file _bPDF _2rda
490	0		_aSolid mechanics and its applications _vvolume 236
500			_aSpringerLink _bSpringer Engineering eBooks 2017 English+International
504			_aIncluye referencias bibliográficas e índice
505	0		_aPreface; Contents; 1 Introduction; Abstract; 1.1 Introduction; 1.2 Development Perspectives; 1.2.1 Increased Damage Growth Resistance of Metal Laminates; 1.2.2 Utilization in Context of Damage Tolerance; 1.2.3 Increasing Strength of Composites; 1.3 From Material Towards Structural Application; 1.4 Contribution to the FML Knowledge; References; 2 Laminate Concepts & Mechanical Properties; Abstract; 2.1 Introduction; 2.2 Aluminium with Epoxy-Based Adhesive Systems; 2.2.1 ARALL and GLARE, Codes and Standardisation; 2.2.2 Aramid Fibres (ARALL); 2.2.3 Glass Fibres (GLARE, Central).
505	8		_a2.2.4 Carbon Fibres (CARE/CARALL)2.2.5 Polymer Fibres (HP-PE, Zylon); 2.2.6 M5 Fibres; 2.3 Other Metal Constituents; 2.3.1 Titanium-Based FMLs; 2.3.2 Stainless Steel-Based FMLs; 2.3.3 Magnesium-Based FMLs; 2.4 Thermoplastic Adhesive Systems; 2.5 Innovative Hybridization Concepts; References; 3 Patents and Intellectual Property; Abstract; 3.1 Introduction; 3.2 Material Concept Development; 3.2.1 Improving Fatigue and Crack Growth; 3.2.2 Improving Impact Resistance and Tolerance; 3.2.3 Thickness Steps; 3.2.4 Thick Panel Concepts for Lower Wing Covers; 3.2.5 Alternative Fuselage Skin Concepts.
505	8		_a3.3 Splicing Concepts3.4 Manufacturing Aspects; 3.4.1 Post-stretching Panels After Curing; 3.4.2 Pre-stretching Panels During Curing; 3.4.3 Lay-up and Curing Concepts; 3.4.4 Alternative Impregnation Processes; 3.5 Design of Fuselage Panels; 3.5.1 General Fuselage Panel Concepts; 3.5.2 Interlaminar Reinforcements and Inserts; 3.5.3 Special Design Features; 3.6 Design of Panel Stiffening Elements; 3.7 FML Components; 3.8 Discussion; 3.8.1 Flat Material Concepts; 3.8.2 Design Aspects; 3.9 Concluding Remarks; References; 4 Stress and Strain; Abstract; 4.1 Introduction.
505	8		_a4.2 Stress-Strain in Orthotropic Materials Under Plane Stress4.3 Classical Laminated Plate Theory; 4.4 Residual Stresses; 4.5 Failure of the Composite Constituent; 4.6 Plasticity of the Metal Constituent; 4.7 Generalized Theories of Plasticity; 4.8 Post-stretching; 4.9 Shear Stress and Strain; 4.10 Out-of-Plane (Bending and Torsion); 4.11 Simple Methods for Design Purposes; 4.11.1 Metal Volume Fraction; 4.11.2 Determination of Shear Properties Using Uniaxial Material Data; 4.12 Limit of Validity of CLT and MVF; References; 5 Blunt Notch Strength; Abstract; 5.1 Introduction.
505	8		_a5.2 Definitions and Failure Phenomena5.2.1 Definitions; 5.2.2 Notch Sensitivity and Ductility; 5.2.3 Biaxial Loading Using Uniaxial Data; 5.2.4 Composite Failure Modes; 5.2.5 Plasticity-Induced Delamination; 5.2.6 Other Failure Phenomena; 5.2.7 Blunt Notch Strength and Ultimate Strength; 5.3 Theoretical Approaches; 5.3.1 Tsai-Hill/Norris Failure Criteria; 5.3.2 Point and Average Stress Criteria; 5.3.3 Blunt Notch Factor to Ultimate Strength in Net Section; 5.4 Applicability to General Loading Conditions; 5.4.1 Uniaxial Off-Axis Loading; 5.4.2 Shear Loading; 5.4.3 Biaxial Loading.
520	3		_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.
650		7	_aMateriales compuestos _xFatigue. _2embne _0(OCoLC)fst00923687 _0 _9141674
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=http://link.springer.com/10.1007/978-3-319-56227-8 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
988			_aEBOOK, asignarmaterias, EBSPRINGER_2017C
998			_b02/2018 _dz _e- _zSI
999			_c95853 _d95853 _x1