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A Finite Element And Experimental Investigation On The Fatigue Of Riveted Lap Joints In Aircraft Applications


A Finite Element And Experimental Investigation On The Fatigue Of Riveted Lap Joints In Aircraft Applications
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Riveted Lap Joints In Aircraft Fuselage


Riveted Lap Joints In Aircraft Fuselage
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Author : Andrzej Skorupa
language : en
Publisher: Springer Science & Business Media
Release Date : 2012-06-23

Riveted Lap Joints In Aircraft Fuselage written by Andrzej Skorupa and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-06-23 with Technology & Engineering categories.


Fatigue of the pressurized fuselages of transport aircraft is a significant problem all builders and users of aircraft have to cope with for reasons associated with assuring a sufficient lifetime and safety, and formulating adequate inspection procedures. These aspects are all addressed in various formal protocols for creating and maintaining airworthiness, including damage tolerance considerations. In most transport aircraft, fatigue occurs in lap joints, sometimes leading to circumstances that threaten safety in critical ways. The problem of fatigue of lap joints has been considerably enlarged by the goal of extending aircraft lifetimes. Fatigue of riveted lap joints between aluminium alloy sheets, typical of the pressurized aircraft fuselage, is the major topic of the present book. The richly illustrated and well-structured chapters treat subjects such as: structural design solutions and loading conditions for fuselage skin joints; relevance of laboratory test results for simple lap joint specimens to riveted joints in a real structure; effect of various production and design related variables on the riveted joint fatigue behaviour; analytical and experimental results on load transmission in mechanically fastened lap joints; theoretical and experimental analysis of secondary bending and its implications for riveted joint fatigue performance; nucleation and shape development of fatigue cracks in riveted longitudinal lap joints; overview of experimental investigations into the multi-site damage for full scale fuselage panels and riveted lap joint specimens; fatigue crack growth and fatigue life prediction methodology for riveted lap joints; residual strength predictions for riveted lap joints in a fuselage structure. The major issues of each chapter are recapitulated in the last section.



A Finite Element And Experimental Investigation On The Fatigue Of Riveted Lap Joints In Aircraft Applications


A Finite Element And Experimental Investigation On The Fatigue Of Riveted Lap Joints In Aircraft Applications
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Author : Amarendra Atre
language : en
Publisher:
Release Date : 2006

A Finite Element And Experimental Investigation On The Fatigue Of Riveted Lap Joints In Aircraft Applications written by Amarendra Atre and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2006 with Airplanes categories.


Aircraft fuselage skin panels are joined together by rivets. The initiation and propagation of fatigue cracks in aircraft structures at and around the rivet/skin interface is directly related to residual stress field induced during the riveting process and subsequent service loads. Variations in the manufacturing process, such as applied loading and presence of sealant can influence the induced residual stress field. In previous research, the riveting process has been simulated by a 2D axisymmetric force-controlled analysis. The 2D analysis cannot capture the unsymmetrical residual stress state resulting from process variations. Experimental work has also been limited to observing effects of squeeze force on fatigue crack initiation in the riveted lap joint. In this work, a 3D finite element model of the riveting process that incorporates plasticity and contact between the various surfaces is simulated using ABAQUS finite element code to capture the residual stress state at the rivet/skin interface. The finite element model is implemented to observe the effects of interference, sealant and hole quality on the residual stress state using Implicit and Explicit solvers. Effects of subsequent load transfer are also analyzed with the developed model. A set of controlled lap joint fatigue experiments for the different conditions provides validation to the model.



Shell Structures Theory And Applications Vol 2


Shell Structures Theory And Applications Vol 2
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Author : Wojciech Pietraszkiewicz
language : en
Publisher: CRC Press
Release Date : 2009-09-22

Shell Structures Theory And Applications Vol 2 written by Wojciech Pietraszkiewicz and has been published by CRC Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2009-09-22 with Technology & Engineering categories.


Shell Structures. Theory and Applications, Volume 2 contains 77 contributions from over 17 countries, reflecting a wide spectrum of scientific and engineering problems of shell structures. The papers are divided into six broad groups: 1. General lectures; 2. Theoretical modeling; 3. Stability; 4. Dynamics; 5. Numerical analysis; 6. Engineering



Proceedings Of The 14th International Conference On The Technology Of Plasticity Current Trends In The Technology Of Plasticity


Proceedings Of The 14th International Conference On The Technology Of Plasticity Current Trends In The Technology Of Plasticity
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Author : Katia Mocellin
language : en
Publisher: Springer Nature
Release Date : 2023-08-28

Proceedings Of The 14th International Conference On The Technology Of Plasticity Current Trends In The Technology Of Plasticity written by Katia Mocellin and has been published by Springer Nature this book supported file pdf, txt, epub, kindle and other format this book has been release on 2023-08-28 with Technology & Engineering categories.


This volume highlights the latest advances, innovations, and applications in the field of metal forming, as presented by leading international researchers and engineers at the 14th International Conference on Technology of Plasticity (ICTP), held in Mandelieu-La Napoule, France on September 24-29, 2023. It covers a diverse range of topics such as manufacturing processes & equipment, materials behavior and characterization, microstructure design by forming, surfaces & interfaces, control & optimization, green / sustainable metal forming technologies, digitalization & AI in metal forming, multi-material processing, agile / flexible metal forming processes, forming of non-metallic materials, micro-forming and luxury applications. The contributions, which were selected by means of a rigorous international peer-review process, present a wealth of exciting ideas that will open novel research directions and foster multidisciplinary collaboration among different specialists.



Comprehensive Structural Integrity Cyclic Loading And Fatigue


Comprehensive Structural Integrity Cyclic Loading And Fatigue
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Author : I. Milne
language : en
Publisher: Elsevier
Release Date : 2003

Comprehensive Structural Integrity Cyclic Loading And Fatigue written by I. Milne and has been published by Elsevier this book supported file pdf, txt, epub, kindle and other format this book has been release on 2003 with Technology & Engineering categories.




Fatigue Durability And Fracture Mechanics


Fatigue Durability And Fracture Mechanics
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Author : S. Seetharamu
language : en
Publisher: Springer Nature
Release Date : 2020-10-01

Fatigue Durability And Fracture Mechanics written by S. Seetharamu and has been published by Springer Nature this book supported file pdf, txt, epub, kindle and other format this book has been release on 2020-10-01 with Science categories.


This book presents selected papers presented during Fatigue Durability India 2019. The contents of this volume discuss advances in the field of fatigue, durability, and fracture, and cover mechanical failure and its applications. The chapters cover a wide spectrum of topics, including design, engineering, testing and computational evaluation of the components or systems for fatigue, durability, and fracture mechanics. The contents of this book will appeal not only to academic researchers, but also to design engineers, failure analysts, maintenance engineers, certification personnel, and R&D professionals involved in a wide variety of industries.



Scientific And Technical Aerospace Reports


Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1995

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Aeronautics categories.




Nasa Sp


Nasa Sp
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Author :
language : en
Publisher:
Release Date : 1993

Nasa Sp written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aeronautics categories.




Aiaa Journal


Aiaa Journal
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Author : American Institute of Aeronautics and Astronautics
language : en
Publisher:
Release Date : 2002

Aiaa Journal written by American Institute of Aeronautics and Astronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with Aeronautics categories.




Analysis And Design Issues For Modern Aerospace Vehicles 1997


Analysis And Design Issues For Modern Aerospace Vehicles 1997
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Author : George J. Simitses
language : en
Publisher:
Release Date : 1997

Analysis And Design Issues For Modern Aerospace Vehicles 1997 written by George J. Simitses and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with Technology & Engineering categories.


This title compiles the 47 papers from the four separate symposia on structural similitude and size effects, thermo mechanical interaction in structures and materials, sandwich structures, and structural and aero-mechanical research in high-cycle fatigue.