| Tag |
First Indicator |
Second Indicator |
Subfields |
| LEADER |
00000cam a2200000 i 4500 |
| 001 |
in00005759613 |
| 005 |
20260407210622.2 |
| 006 |
m o d |
| 007 |
cr cnu|||unuuu |
| 008 |
150914t20152016enk ob 001 0 eng d |
| 019 |
|
|
|a 929521523
|a 933212289
|a 949653232
|
| 020 |
|
|
|a 9780124104419
|q (electronic bk.)
|
| 020 |
|
|
|a 012410441X
|q (electronic bk.)
|
| 020 |
|
|
|a 0124096050
|
| 020 |
|
|
|a 9780124096059
|
| 020 |
|
|
|z 9780124096059
|
| 035 |
|
|
|a (OCoLC)921142877
|z (OCoLC)929521523
|z (OCoLC)933212289
|z (OCoLC)949653232
|
| 040 |
|
|
|a N$T
|b eng
|e rda
|e pn
|c N$T
|d OPELS
|d N$T
|d YDXCP
|d IDEBK
|d CDX
|d EBLCP
|d KNOVL
|d REB
|d ZCU
|d COO
|d UAB
|d OCLCQ
|d DKU
|d U3W
|d D6H
|d OCLCF
|d OCLCQ
|d CEF
|d RRP
|d OCLCQ
|d KKS
|d OCLCQ
|d S2H
|d OCLCO
|d OCLCQ
|d OCLCO
|d OCLCQ
|
| 049 |
|
|
|a TXAM
|
| 050 |
|
4 |
|a TA656.6
|
| 066 |
|
|
|c (S
|
| 072 |
|
7 |
|a TEC
|x 009000
|2 bisacsh
|
| 072 |
|
7 |
|a TEC
|x 035000
|2 bisacsh
|
| 082 |
0 |
4 |
|a 620.1/187
|2 23
|
| 100 |
1 |
|
|a Giurgiutiu, Victor,
|e author.
|
| 245 |
1 |
0 |
|a Structural health monitoring of aerospace composites /
|c Victor Giurgiutiu.
|
| 264 |
|
1 |
|a London, UK :
|b Academic Press is an imprint of Elsevier,
|c [2015]
|
| 264 |
|
4 |
|c ©2016
|
| 300 |
|
|
|a 1 online resource
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a computer
|b c
|2 rdamedia
|
| 338 |
|
|
|a online resource
|b cr
|2 rdacarrier
|
| 500 |
|
|
|a Includes index.
|
| 588 |
0 |
|
|a Online resource; title from title details screen (ScienceDirect, viewed September 16, 2015).
|
| 505 |
0 |
|
|a Front Cover; Structural Health Monitoring of Aerospace Composites; Copyright Page; Dedication; Contents; 1 Introduction; 1.1 Preamble; 1.2 Why Aerospace Composites?; 1.3 What are Aerospace Composites?; 1.3.1 Definition of Aerospace Composites; 1.3.2 High-Performance Fibers for Aerospace Composites Applications; 1.3.3 High-Performance Matrices for Aerospace Composites Applications; 1.3.4 Advantages of Composites in Aerospace Usage; 1.3.5 Fabrication of Aerospace Composites; 1.4 Evolution of Aerospace Composites; 1.4.1 Early Advances; 1.4.2 Composite Growth in the 1960s and 1970s.
|
| 505 |
8 |
|
|a 1.4.3 Composites Growth Since the 1980s1.5 Today's Aerospace Composites; 1.5.1 Boeing 787 Dreamliner; 1.5.2 Airbus A350 XWB; 1.6 Challenges for Aerospace Composites; 1.6.1 Concerns About the Aerospace Use of Composites; 1.6.2 The November 2001 Accident of AA Flight 587; 1.6.3 Fatigue Behavior of Composite Materials; 1.6.4 The Future of Composites in Aerospace; 1.7 About This Book; References; 2 Fundamentals of Aerospace Composite Materials; 2.1 Introduction; 2.2 Anisotropic Elasticity; 2.2.1 Basic Notations; 2.2.2 Stresses-The Stress Tensor.
|
| 505 |
8 |
|
|a 2.2.3 Strain-Displacement Relations-The Strain Tensor2.2.4 Stress-Strain Relations; 2.2.4.1 Stiffness Tensor; Compliance Tensor; 2.2.4.2 From Tensor Notations to Voigt Matrix Notation; 2.2.4.3 Stiffness Matrix; 2.2.4.4 Compliance Matrix; 2.2.4.5 Stress-Strain Relations for an Isotropic Material; 2.2.5 Equation of Motion in Terms of Stresses; 2.2.6 Equation of Motion in Terms of Displacements; 2.3 Unidirectional Composite Properties; 2.3.1 Elastic Constants of a Unidirectional Composite; 2.3.2 Compliance Matrix of a Unidirectional Composite.
|
| 505 |
8 |
|
|a 2.4.4 Rotated 2D Compliance Matrix2.4.5 Proof of RTR-1=T-t; 2.5 Fully 3D Elastic Properties of a Composite Layer; 2.5.1 Orthotropic Stiffness Matrix; 2.5.2 Rotated Stiffness Matrix; 2.5.3 Equations of Motion for a Monoclinic Composite Layer; 2.5.4 Rotated Compliance Matrix; 2.5.5 Note on the Use of Closed-Form Expression in the C and S matrices; 2.5.6 Proof of RTR-1=T-t in 3D; 2.6 Problems and Exercises; References; 3 Vibration of Composite Structures; 3.1 Introduction; 3.1.1 Displacements for Axial-Flexural Vibration of Composite Plates; 3.1.2 Stress Resultants.
|
| 520 |
8 |
|
|a Annotation
|b "Structural Health Monitoring of Aerospace Composite Structures" offers a comprehensive review of established and promising technologies under development in the emerging area of structural health monitoring (SHM) of aerospace composite structures. Beginning with a description of the different types of composite damage, which differ fundamentally from the damage states encountered in metallic airframes, the book moves on to describe the SHM methods and sensors currently under consideration before considering application examples related to specific composites, SHM sensors, and detection methods. Expert author Victor Giurgiutiu closes with a valuable discussion of the advantages and limitations of various sensors and methods, helping you to make informed choices in your structure research and development. The first comprehensive review of one of the most ardent research areas in aerospace structures, providing breadth and detail to bring engineers and researchers up to speed on this rapidly developing fieldCovers the main classes of SHM sensors, including fiber optic sensors, piezoelectric wafer active sensors, electrical properties sensors and conventional resistance strain gauges, and considers their applications and limitationIncludes details of active approaches, including acousto-ultrasonics, vibration, frequency transfer function, guided-wave tomography, phased arrays, and electrochemical impedance spectroscopy (ECIS), among other emerging methods
|
| 504 |
|
|
|a Includes bibliographical references at the end of each chapters and index.
|
| 650 |
|
0 |
|a Structural health monitoring.
|
| 650 |
|
0 |
|a Composite materials
|x Nondestructive testing.
|
| 650 |
|
6 |
|a Surveillance de l'état des structures.
|
| 650 |
|
6 |
|a Composites
|x Contrôle non destructif.
|
| 650 |
|
7 |
|a TECHNOLOGY & ENGINEERING
|x Engineering (General)
|2 bisacsh
|
| 650 |
|
7 |
|a TECHNOLOGY & ENGINEERING
|x Reference.
|2 bisacsh
|
| 650 |
|
7 |
|a Structural health monitoring
|2 fast
|
| 655 |
|
7 |
|a Electronic books.
|2 local
|
| 710 |
2 |
|
|a ScienceDirect (Online service)
|
| 776 |
0 |
8 |
|i Print version:
|a Giurgiutiu, Victor.
|t Structural Health Monitoring of Aerospace Composites.
|d Saint Louis : Elsevier Science, ©2015
|z 9780124096059
|
| 856 |
4 |
0 |
|u http://proxy.library.tamu.edu/login?url=https://www.sciencedirect.com/science/book/9780124096059
|z Connect to the full text of this electronic book
|t 0
|
| 880 |
8 |
|
|6 505-00/(S
|a 2.3.3 Stiffness Matrix of a Unidirectional Composite; 2.3.4 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.
|
| 955 |
|
|
|a Elsevier ScienceDirect 2026-2027
|
| 955 |
|
|
|a Knovel ebooks
|
| 994 |
|
|
|a 92
|b TXA
|
| 999 |
f |
f |
|s 3c33ec7b-f4fb-403d-846d-67f5454b4607
|i 33d335d1-482e-4456-ab26-3248e57aa234
|t 0
|
| 952 |
f |
f |
|a Texas A&M University
|b College Station
|c Electronic Resources
|s www_evans
|d Available Online
|t 0
|e TA656.6
|h Library of Congress classification
|
| 998 |
f |
f |
|a TA656.6
|t 0
|l Available Online
|