Damage Growth in Aerospace Composites (Record no. 54526)

000 -LEADER
fixed length control field 03715nam a22005055i 4500
001 - CONTROL NUMBER
control field 978-3-319-04004-2
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20200421111653.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 150107s2015 gw | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783319040042
-- 978-3-319-04004-2
082 04 - CLASSIFICATION NUMBER
Call Number 629.1
245 10 - TITLE STATEMENT
Title Damage Growth in Aerospace Composites
300 ## - PHYSICAL DESCRIPTION
Number of Pages VI, 279 p. 210 illus., 14 illus. in color.
490 1# - SERIES STATEMENT
Series statement Springer Aerospace Technology,
505 0# - FORMATTED CONTENTS NOTE
Remark 2 Introduction -- Detailed methodologies for integrated delamination growth and fiber-matrix damage progression simulation -- Delamination Growth in Composite Plates under Fatigue Loading Conditions -- Influence of intralaminar damage on the delamination crack evolution -- Microdamage modeling in laminates -- Finite element study of delaminations in notched composites -- Effect of the damage extension through the thickness on the calculation of the residual strength of impacted composite laminates -- A Fast Numerical Methodology for Delamination Growth Initiation Simulation -- An Experimental Study on the strength of out of plane loaded composite structures -- Buckling and collapse tests using advanced measurement systems -- Vacuum infusion manufacturing of CFRP panels with induced delamination -- Lock-in Thermography to detect delamination in Carbon Fibers Reinforced Polymers (Carosena Meola and Giovanni M. Carlomagno).
520 ## - SUMMARY, ETC.
Summary, etc This book presents novel methods for the simulation of damage evolution in aerospace composites that will assist in predicting damage onset and growth and thus foster less conservative designs which realize the promised economic benefits of composite materials. The presented integrated numerical/experimental methodologies are capable of taking into account the presence of damage and its evolution in composite structures from the early phases of the design (conceptual design) through to the detailed finite element method analysis and verification phase. The book is based on the GARTEUR Research Project AG-32, which ran from 2007 to 2012, and documents the main results of that project. In addition, the state of the art in European projects on damage evolution in composites is reviewed. While the high specific strength and stiffness of composite materials make them suitable for aerospace structures, their sensitivity to damage means that designing with composites is a challenging task. The new approaches described here will prove invaluable in meeting that challenge.
700 1# - AUTHOR 2
Author 2 Riccio, Aniello.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier http://dx.doi.org/10.1007/978-3-319-04004-2
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Cham :
-- Springer International Publishing :
-- Imprint: Springer,
-- 2015.
336 ## -
-- text
-- txt
-- rdacontent
337 ## -
-- computer
-- c
-- rdamedia
338 ## -
-- online resource
-- cr
-- rdacarrier
347 ## -
-- text file
-- PDF
-- rda
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Continuum mechanics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Astronautics.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace Technology and Astronautics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Ceramics, Glass, Composites, Natural Methods.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Continuum Mechanics and Mechanics of Materials.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
-- 1869-1730
912 ## -
-- ZDB-2-ENG

No items available.