Constitutive Relations under Impact Loadings (Record no. 53386)

000 -LEADER
fixed length control field 03149nam a22005415i 4500
001 - CONTROL NUMBER
control field 978-3-7091-1768-2
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20200421111153.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 131219s2014 au | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783709117682
-- 978-3-7091-1768-2
082 04 - CLASSIFICATION NUMBER
Call Number 620.1
245 10 - TITLE STATEMENT
Title Constitutive Relations under Impact Loadings
Sub Title Experiments, Theoretical and Numerical Aspects /
250 ## - EDITION STATEMENT
Edition statement 1.
300 ## - PHYSICAL DESCRIPTION
Number of Pages VII, 285 p. 140 illus.
490 1# - SERIES STATEMENT
Series statement CISM International Centre for Mechanical Sciences,
505 0# - FORMATTED CONTENTS NOTE
Remark 2 Testing with bars from dynamic to quasi-static -- Dynamic testing of materials -- Material behavior under dynamics loading, modeling and experiments -- Analysis of some high-speed impact problems in the aircraft industry -- Computer estimation of plastic strain localization and failure for large strain rates using viscoplasticity -- Inelastic flow and failure of metallic solids accounting for asymmetry of elastic range and micro-shear banding.
520 ## - SUMMARY, ETC.
Summary, etc The book describes behavior of materials (ductile, brittle and composites) under impact loadings and high strain rates. The three aspects: experimental, theoretical and numerical are in the focus of interest. Hopkinson bars are mainly used as experimental devices to describe dynamic behavior of materials. The precise description of experimental techniques and interpretation of wave interaction are carefully discussed. Theoretical background refers to rate dependent thermoviscoplastic formulation. This includes the discussion of well posedness of initial boundary value problems and the solution of the system of governing equations using numerical methods. Explicit time integration is used in computations to solve dynamic problems. In addition, many applications in aeronautic and automotive industries are exposed.
700 1# - AUTHOR 2
Author 2 �odygowski, Tomasz.
700 1# - AUTHOR 2
Author 2 Rusinek, Alexis.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier http://dx.doi.org/10.1007/978-3-7091-1768-2
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Vienna :
-- Springer Vienna :
-- Imprint: Springer,
-- 2014.
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-- txt
-- rdacontent
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-- computer
-- c
-- rdamedia
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-- online resource
-- cr
-- rdacarrier
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-- text file
-- PDF
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650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Continuum mechanics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Structural mechanics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Materials science.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Continuum Mechanics and Mechanics of Materials.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Characterization and Evaluation of Materials.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Structural Mechanics.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
-- 0254-1971 ;
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-- ZDB-2-ENG

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