000			03909nam a2200313 i 4500
001			43738
008			150914t20152016enk 001 0 eng d
020			_a9780124104419 _qelectronic bk.
020			_a012410441X _qelectronic bk.
020			_a9780124096059. _qhardback
035			_a(OCoLC)921142877 _z(OCoLC)929521523
040			_aN$T _beng _erda _epn _cN$T _dOPELS _dN$T _dYDXCP _dIDEBK _dCDX _dEBLCP _dKNOVL _dBAUN
049			_aBAUN_MERKEZ
050		4	_aTA656.6 _b.G587 2016
100	1		_aGiurgiutiu, Victor,
245	1	0	_aStructural health monitoring of aerospace composites / _cVictor Giurgiutiu.
264		1	_aLondon, UK : _bAcademic Press is an imprint of Elsevier, _c[2015].
264		4	_c©2016.
300			_a457 pages : _billustrations ; _c24 cm
336			_atext _btxt _2rdacontent.
337			_aunmediated _bx _2rdamedia.
338			_avolume _bvf _2rdacarrier.
500			_aIncludes index.
505	0		_tFront Cover _tStructural Health Monitoring of Aerospace Composites _tCopyright Page _tDedication _tContents _t1 Introduction _t1.1 Preamble _t1.2 Why Aerospace Composites? _t1.3 What are Aerospace Composites? _t1.3.1 Definition of Aerospace Composites _t1.3.2 High-Performance Fibers for Aerospace Composites Applications _t1.3.3 High-Performance Matrices for Aerospace Composites Applications _t1.3.4 Advantages of Composites in Aerospace Usage _t1.3.5 Fabrication of Aerospace Composites _t1.4 Evolution of Aerospace Composites _t1.4.1 Early Advances _t1.4.2 Composite Growth in the 1960s and 1970s. _t1.4.3 Composites Growth Since the 1980s1.5 Today's Aerospace Composites _t1.5.1 Boeing 787 Dreamliner _t1.5.2 Airbus A350 XWB _t1.6 Challenges for Aerospace Composites _t1.6.1 Concerns About the Aerospace Use of Composites _t1.6.2 The November 2001 Accident of AA Flight 587 _t1.6.3 Fatigue Behavior of Composite Materials _t1.6.4 The Future of Composites in Aerospace _t1.7 About This Book _tReferences _t2 Fundamentals of Aerospace Composite Materials _t2.1 Introduction _t2.2 Anisotropic Elasticity _t2.2.1 Basic Notations _t2.2.2 Stresses-The Stress Tensor. _t2.2.3 Strain-Displacement Relations-The Strain Tensor2.2.4 Stress-Strain Relations _t2.2.4.1 Stiffness Tensor _tCompliance Tensor _t2.2.4.2 From Tensor Notations to Voigt Matrix Notation _t2.2.4.3 Stiffness Matrix _t2.2.4.4 Compliance Matrix _t2.2.4.5 Stress-Strain Relations for an Isotropic Material _t2.2.5 Equation of Motion in Terms of Stresses _t2.2.6 Equation of Motion in Terms of Displacements _t2.3 Unidirectional Composite Properties _t2.3.1 Elastic Constants of a Unidirectional Composite _t2.3.2 Compliance Matrix of a Unidirectional Composite. _t2.4.4 Rotated 2D Compliance Matrix2.4.5 Proof of RTR-1=T-t _t2.5 Fully 3D Elastic Properties of a Composite Layer _t2.5.1 Orthotropic Stiffness Matrix _t2.5.2 Rotated Stiffness Matrix _t2.5.3 Equations of Motion for a Monoclinic Composite Layer _t2.5.4 Rotated Compliance Matrix _t2.5.5 Note on the Use of Closed-Form Expression in the C and S matrices _t2.5.6 Proof of RTR-1=T-t in 3D _t2.6 Problems and Exercises _tReferences _t3 Vibration of Composite Structures _t3.1 Introduction _t3.1.1 Displacements for Axial-Flexural Vibration of Composite Plates _t3.1.2 Stress Resultants.
650		0	_aStructural health monitoring.
650		0	_aComposite materials _xNondestructive testing.
880	8		_6505-01/(S _a2.3.3 Stiffness Matrix of a Unidirectional Composite2.3.4 Estimation of Elastic Constants from the Constituent Properties; 2.3.4.1 Estimation of the Longitudinal Modulus EL; 2.3.4.2 Estimation of the Transverse Modulus ET; 2.3.4.3 Estimation of Poisson Ratio νLT; 2.3.4.4 Estimation of the LT Shear Modulus GLT; 2.3.4.5 Estimation of Transverse Shear Modulus G23; 2.3.4.6 Matrix-Dominated Approximations; 2.4 Plane-Stress 2D Elastic Properties of a Composite Layer; 2.4.1 Plane-Stress 2D Compliance Matrix; 2.4.2 Plane-Stress 2D Stiffness Matrix; 2.4.3 Rotated 2D Stiffness Matrix.
942			_2lcc _cKT
999			_c41419 _d41419