Coverart for item
The Resource Damage tolerance of metallic aircraft structures : materials and numerical modelling, Sérgio M. O. Tavares, Paulo M.S.T. de Castro

Damage tolerance of metallic aircraft structures : materials and numerical modelling, Sérgio M. O. Tavares, Paulo M.S.T. de Castro

Label
Damage tolerance of metallic aircraft structures : materials and numerical modelling
Title
Damage tolerance of metallic aircraft structures
Title remainder
materials and numerical modelling
Statement of responsibility
Sérgio M. O. Tavares, Paulo M.S.T. de Castro
Creator
Contributor
Subject
Language
eng
Member of
http://library.link/vocab/creatorName
Tavares, Sérgio M. O.,
Dewey number
629.13431
Index
index present
Literary form
non fiction
Nature of contents
  • dictionaries
  • bibliography
http://library.link/vocab/relatedWorkOrContributorDate
1950-
http://library.link/vocab/relatedWorkOrContributorName
Castro, Paulo M. S. Tavares de
Series statement
SpringerBriefs in applied sciences and technology. Computational mechanics
http://library.link/vocab/subjectName
  • Airframes
  • Fracture mechanics
  • Metals
  • Airframes
Label
Damage tolerance of metallic aircraft structures : materials and numerical modelling, Sérgio M. O. Tavares, Paulo M.S.T. de Castro
Instantiates
Publication
Antecedent source
unknown
Bibliography note
Includes bibliographical references and index
Color
multicolored
Contents
  • Intro; Preface; Contents; Acronyms and Symbols; Part I Damage Tolerance of Aircraft Structures; 1 Introduction; 1.1 Evolution of Fatigue Design Approaches; 1.2 Cracks and Damage; References; 2 Maintenance; References; 3 Fatigue Crack Growth; 3.1 Life Estimation and Scatter; 3.2 Improvement of Fatigue Strength; References; 4 Materials; 4.1 Introductory Remarks; 4.2 Aluminium-Lithium; 4.3 Titanium; 4.4 Fibre Metal Laminates-FMLs; 4.5 Polymeric Composites; References; 5 Widespread Fatigue Damage and Limit of Validity; 5.1 Evolution of Regulations; 5.2 A Glance into Technical Aspects
  • 5.2.1 Structural Analyses5.2.2 Integral Structures; Crenellations; 5.2.3 Morphing; References; Part II Design of Monolithic Aeronautical Structures; 6 Alloys and Fatigue Crack Propagation; References; 7 Residual Stress; 7.1 Introduction and Experimental Measurement; 7.2 Welding and Numerical Modelling; 7.2.1 Introduction; 7.2.2 Case Study: Laser Beam Welded Butt Joints of Thin Al Alloy Plates; 7.2.3 Case Study: T-Joint; References; 8 Fatigue Crack Propagation of a Structural Detail; 8.1 Introduction; 8.2 Fatigue Crack Growth Laws; 8.2.1 Parameters for the Crack Growth Laws
  • 8.2.2 Consideration of Residual Stress Effects8.3 Finite Element Modelling; 8.3.1 Discussion and Conclusions; References; Index
Control code
on1048355809
Dimensions
unknown
Extent
1 online resource
File format
unknown
Form of item
online
Isbn
9783319701905
Level of compression
unknown
Note
SpringerLink
Quality assurance targets
not applicable
Reformatting quality
unknown
Sound
unknown sound
Specific material designation
remote
System control number
(OCoLC)1048355809
Label
Damage tolerance of metallic aircraft structures : materials and numerical modelling, Sérgio M. O. Tavares, Paulo M.S.T. de Castro
Publication
Antecedent source
unknown
Bibliography note
Includes bibliographical references and index
Color
multicolored
Contents
  • Intro; Preface; Contents; Acronyms and Symbols; Part I Damage Tolerance of Aircraft Structures; 1 Introduction; 1.1 Evolution of Fatigue Design Approaches; 1.2 Cracks and Damage; References; 2 Maintenance; References; 3 Fatigue Crack Growth; 3.1 Life Estimation and Scatter; 3.2 Improvement of Fatigue Strength; References; 4 Materials; 4.1 Introductory Remarks; 4.2 Aluminium-Lithium; 4.3 Titanium; 4.4 Fibre Metal Laminates-FMLs; 4.5 Polymeric Composites; References; 5 Widespread Fatigue Damage and Limit of Validity; 5.1 Evolution of Regulations; 5.2 A Glance into Technical Aspects
  • 5.2.1 Structural Analyses5.2.2 Integral Structures; Crenellations; 5.2.3 Morphing; References; Part II Design of Monolithic Aeronautical Structures; 6 Alloys and Fatigue Crack Propagation; References; 7 Residual Stress; 7.1 Introduction and Experimental Measurement; 7.2 Welding and Numerical Modelling; 7.2.1 Introduction; 7.2.2 Case Study: Laser Beam Welded Butt Joints of Thin Al Alloy Plates; 7.2.3 Case Study: T-Joint; References; 8 Fatigue Crack Propagation of a Structural Detail; 8.1 Introduction; 8.2 Fatigue Crack Growth Laws; 8.2.1 Parameters for the Crack Growth Laws
  • 8.2.2 Consideration of Residual Stress Effects8.3 Finite Element Modelling; 8.3.1 Discussion and Conclusions; References; Index
Control code
on1048355809
Dimensions
unknown
Extent
1 online resource
File format
unknown
Form of item
online
Isbn
9783319701905
Level of compression
unknown
Note
SpringerLink
Quality assurance targets
not applicable
Reformatting quality
unknown
Sound
unknown sound
Specific material designation
remote
System control number
(OCoLC)1048355809

Library Locations

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