Subsurface Fatigue Crack Growth in Glare Fibre Metal Laminates

Subsurface Fatigue Crack Growth in Glare Fibre Metal Laminates PDF Author: Christian Eugene Randell
Publisher:
ISBN: 9789081025713
Category :
Languages : en
Pages :

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Subsurface Fatigue Crack Growth in Glare Fibre Metal Laminates

Subsurface Fatigue Crack Growth in Glare Fibre Metal Laminates PDF Author: Christian Eugene Randell
Publisher:
ISBN: 9789081025713
Category :
Languages : en
Pages :

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On Subsurface Crack Growth in Fibre Metal Laminate Materials

On Subsurface Crack Growth in Fibre Metal Laminate Materials PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

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Book Description
Fatigue crack growth in fibre metal laminates (FMLs) is significantly more complex than in monolithic materials due to the interaction of various physical mechanisms that govern the growth of cracks in laminates. Extensive research has gone into the development of analytical models that try to predict the growth of surface and through-cracks in the FML Glare under fatigue loading. To date, less emphasis has been placed on developing fatigue crack growth models for part through cracks. These part through cracks exhibit different rates of growth for each layer of the laminate based upon differing stress levels and delamination zone sizes. To better predict the residual strength of FML structures, understanding the behavior of subsurface crack growth is required. For this reason, data of crack growth rates for layers of various laminates were compared to an analytical fatigue crack growth model developed for surface cracks in a specific type of FML, Glare. This paper gives an initial assessment of the model's veracity for subsurface crack growth.

Fatigue and Fracture of Fibre Metal Laminates

Fatigue and Fracture of Fibre Metal Laminates PDF Author: René Alderliesten
Publisher: Springer
ISBN: 3319562274
Category : Technology & Engineering
Languages : en
Pages : 310

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Book Description
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.

ตําราสรีรวิทยา

ตําราสรีรวิทยา PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Fatigue Crack Propagation and Delamination Growth in Glare

Fatigue Crack Propagation and Delamination Growth in Glare PDF Author: R. Alderliesten
Publisher: Delft University Press
ISBN: 9789040725883
Category : Science
Languages : en
Pages : 188

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Fatigue Crack Growth in Fiber Metal Laminates

Fatigue Crack Growth in Fiber Metal Laminates PDF Author: Per Hofslagare
Publisher:
ISBN: 9789173738941
Category : Metallic composites
Languages : en
Pages : 114

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Fatigue Crack and Delamination Growth in Fibre Metal Laminates Under Variable Amplitude Loading

Fatigue Crack and Delamination Growth in Fibre Metal Laminates Under Variable Amplitude Loading PDF Author: Sharifullah Khan
Publisher:
ISBN: 9789088915550
Category :
Languages : en
Pages :

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Composite Joints and Connections

Composite Joints and Connections PDF Author: P Camanho
Publisher: Elsevier
ISBN: 0857094920
Category : Technology & Engineering
Languages : en
Pages : 537

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Book Description
The growing use of composites over metals for structural applications has made a thorough understanding of the behaviour of composite joints in various applications essential for engineers, but has also presented them with a new set of problems. Composite joints and connections addresses these differences and explores the design, modelling and testing of bonded and bolted joints and connections.Part one discusses bolted joints whilst part two examines bonded joints. Chapters review reinforcement techniques and applications for composite bolted and bonded joints and investigate the causes and effects of fatigue and stress on both types of joint in various applications and environments. Topics in part one include metal hybridization, glass-reinforced aluminium (GLARE), hybrid fibre metal laminates (FML), glass fibre reinforced polymer (GFRP) and carbon fibre reinforced polymer (CFRP) composites. Topics in part two include calculation of strain energy release rates, simulating fracture and fatigue failure using cohesive zone models, marine and aerospace applications, advanced modelling, stress analysis of bonded patches and scarf repairs.Composite joints and connections is a valuable reference for composite manufacturers and composite component fabricators, the aerospace, automotive, shipbuilding and civil engineering industries and for anyone involved in the joining and repair of composite structures. - Explores the design, modelling and testing of bonded and bolted joints and connections - Reviews reinforcement techniques and applications for composite bolted and bonded joints - Investigates the causes and effects of fatigue and stress on bolted and bonded joints in various applications and environments

Effect of Fiber Reinforcement on Fatigue Crack Growth in Fiber Metal Laminates

Effect of Fiber Reinforcement on Fatigue Crack Growth in Fiber Metal Laminates PDF Author: Per Hofslagare
Publisher:
ISBN: 9789173734684
Category :
Languages : en
Pages : 71

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Fibre Metal Laminates

Fibre Metal Laminates PDF Author: Ad Vlot
Publisher: Springer Science & Business Media
ISBN: 9401009953
Category : Technology & Engineering
Languages : en
Pages : 509

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Book Description
Fibre metal laminates were developed at Delft University of Technology in The Netherlands, from the beginning of the 1980s. This is a new family of hybrid materials consisting of thin metal layers bonded together by fibres embedded in an adhesive. As a result of this build-up, fibre metal laminates possess a mixture of the characteristics of both metals and composite materials. Initial development led to the `Arall' variant using aramid fibres, which was first applied on the C-17 military transport aircraft around 1990. Large-scale application became possible with a variant using glass fibres, dubbed `Glare', which was selected for the Airbus A380 super jumbo in 2001. This is the first book to discuss these new materials and it deals mostly with Glare. It covers most of the relevant aspects of the materials, from static mechanical properties, fatigue and impact to design, production and maintenance of aircraft structures. This book contains the basic information on these new materials necessary for engineers and aircraft operators alike.