Structural Analysis of Composite Wind Turbine Blades (Record no. 57746)

000 -LEADER
fixed length control field 03628nam a22005175i 4500
001 - CONTROL NUMBER
control field 978-3-319-00864-6
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20200421112227.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 130704s2013 gw | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783319008646
-- 978-3-319-00864-6
082 04 - CLASSIFICATION NUMBER
Call Number 621.042
100 1# - AUTHOR NAME
Author Chortis, Dimitris I.
245 10 - TITLE STATEMENT
Title Structural Analysis of Composite Wind Turbine Blades
Sub Title Nonlinear Mechanics and Finite Element Models with Material Damping /
300 ## - PHYSICAL DESCRIPTION
Number of Pages XIII, 235 p.
490 1# - SERIES STATEMENT
Series statement Research Topics in Wind Energy,
505 0# - FORMATTED CONTENTS NOTE
Remark 2 From the Contents: Historical Review on the Linear and Nonlinear Damped Structural Behavior of Composite Structures -- Linear Material Coupling Effect on Structural Damping of Composite Beams and Blades -- Nonlinear Damping Mechanics and Finite Element Model for the Static and Damped Free-Vibration Analysis of Composite Strips -- Nonlinear Dynamic Response of Composite Plate-Beams -- Prediction of Nonlinear Damped Response of Large-Scale Blade Composite Structures.
520 ## - SUMMARY, ETC.
Summary, etc This book concerns the development of novel finite elements for the structural analysis of composite beams and blades. The introduction of material damping is also an important aspect of composite structures and it is presented here in terms of their static and dynamic behavior. The book thoroughly presents a new shear beam finite element, which entails new blade section mechanics, capable of predicting structural blade coupling due to composite coupling and/or internal section geometry. Theoretical background is further expanded towards the inclusion of nonlinear structural blade models and damping mechanics for composite structures. The models effectively include geometrically nonlinear terms due to large displacements and rotations, improve the modeling accuracy of very large flexible blades, and enable the modeling of rotational stiffening and buckling, as well as, nonlinear structural coupling. Validation simulations on specimen level study the geometric nonlinearities effect on the modal frequencies and damping values of composite strips of various angle-ply laminations under either tensile or buckling loading. A series of correlation cases between numerical predictions and experimental measurements give credence to the developed nonlinear beam finite element models and underline the essential role of new nonlinear damping and stiffness terms.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier http://dx.doi.org/10.1007/978-3-319-00864-6
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Heidelberg :
-- Springer International Publishing :
-- Imprint: Springer,
-- 2013.
336 ## -
-- text
-- txt
-- rdacontent
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-- 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
-- Renewable energy resources.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Complexity, Computational.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Renewable energy sources.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Alternate energy sources.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Green energy industries.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Renewable and Green Energy.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Renewable and Green Energy.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Complexity.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
-- 2196-7806 ;
912 ## -
-- ZDB-2-ENG

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