Fatigue and Fracture of Fibre Metal Laminates (Record no. 75986)
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000 -LEADER | |
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fixed length control field | 03473nam a22005535i 4500 |
001 - CONTROL NUMBER | |
control field | 978-3-319-56227-8 |
005 - DATE AND TIME OF LATEST TRANSACTION | |
control field | 20220801214127.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
fixed length control field | 170420s2017 sz | s |||| 0|eng d |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
ISBN | 9783319562278 |
-- | 978-3-319-56227-8 |
082 04 - CLASSIFICATION NUMBER | |
Call Number | 620.1 |
100 1# - AUTHOR NAME | |
Author | Alderliesten, René. |
245 10 - TITLE STATEMENT | |
Title | Fatigue and Fracture of Fibre Metal Laminates |
250 ## - EDITION STATEMENT | |
Edition statement | 1st ed. 2017. |
300 ## - PHYSICAL DESCRIPTION | |
Number of Pages | XII, 300 p. 189 illus., 116 illus. in color. |
490 1# - SERIES STATEMENT | |
Series statement | Solid Mechanics and Its Applications, |
505 0# - FORMATTED CONTENTS NOTE | |
Remark 2 | I Laminate concepts and properties -- 1 Introduction -- 2 Intellectual property and patents -- 3 Laminate concepts and typical properties -- II Prediction & analysis methods -- 1 Stress-train -- 2 Blunt notch strength -- 3 Bearing strength -- 4 Fatigue initiation -- 5 Static and fatigue delamination -- 6 Fatigue crack propagation -- 7 Residual strength -- III Environmental aspects -- 1 Temperature -- 2 Effect of frequency (wave form, hold time) -- 3 Acoustic fatigue. |
520 ## - SUMMARY, ETC. | |
Summary, etc | This book contributes to the field of hybrid technology, describing the current state of knowledge concerning the hybrid material concept of laminated metallic and composite sheets for primary aeronautical structural applications. It is the only book to date on fatigue and fracture of fibre metal laminates (FMLs). The first section of the book provides a general background of the FML technology, highlighting the major FML types developed and studied over the past decades in conjunction with an overview of industrial developments based on filed patents. In turn, the second section discusses the mechanical response to quasi-static loading, together with the fracture phenomena during quasi-static and cyclic loading. To consider the durability aspects related to strength justification and certification of primary aircraft structures, the third section discusses thermal aspects related to FMLs and their mechanical response to various environmental and acoustic conditions. |
856 40 - ELECTRONIC LOCATION AND ACCESS | |
Uniform Resource Identifier | https://doi.org/10.1007/978-3-319-56227-8 |
942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
Koha item type | eBooks |
264 #1 - | |
-- | Cham : |
-- | Springer International Publishing : |
-- | Imprint: Springer, |
-- | 2017. |
336 ## - | |
-- | text |
-- | txt |
-- | rdacontent |
337 ## - | |
-- | computer |
-- | c |
-- | rdamedia |
338 ## - | |
-- | online resource |
-- | cr |
-- | rdacarrier |
347 ## - | |
-- | text file |
-- | |
-- | rda |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Mechanics, Applied. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Materials—Analysis. |
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 Mechanics. |
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Characterization and Analytical Technique. |
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Aerospace Technology and Astronautics. |
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE | |
-- | 2214-7764 ; |
912 ## - | |
-- | ZDB-2-ENG |
912 ## - | |
-- | ZDB-2-SXE |
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