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ICAF 2009, Bridging the Gap between Theory and Operational Practice

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Cover of 'ICAF 2009, Bridging the Gap between Theory and Operational Practice'

Table of Contents

  1. Altmetric Badge
    Book Overview
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    Chapter 1 A Test Concept For Future Aircraft Fuselage Panels
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    Chapter 2 Marker Loads for Quantitative Fractography of Fatigue Cracks in Aerospace Alloys
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    Chapter 3 Substantiations of an Airborne Composite Radome Mounted on an Aircraft Dome
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    Chapter 4 Development of a “Low Stress Criterion” That Eliminate a Large Portion of the Aircraft from Damage Tolerance Based Maintenance Program for Structural Repairs Required by the New Part 26 Federal Regulation
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    Chapter 5 Damage Tolerance Philosophy for Bonded Aircraft Structures
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    Chapter 6 First Diamond
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    Chapter 7 Survey of Structural Repairs and Alterations in Transport Category Airplanes
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    Chapter 8 Enhanced Teardown of Ex-Service F/A-18A/B/C/D Centre Fuselages
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    Chapter 9 Glare Teardowns From the Megaliner Barrel (Mlb) Fatigue Test
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    Chapter 10 30 Years of Damage Tolerance – Have we Got it Right?
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    Chapter 11 Compilation Of Damage Findings From Multiple Recent Teardown Analysis Programs
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    Chapter 12 Detection Of Arrested Crack For Foam Core Sandwich Structures Using Optical Fiber Sensors Embedded In A Crack Arrester
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    Chapter 13 Concept Of The New A320 Fatigue Test
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    Chapter 14 The Use Of Composite Material Strips To Extend The Damage-Tolerance Life Of Integrally Stiffened Aluminum Panels
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    Chapter 15 Structural Integrity Of A Wing Upper Skin With Exfoliation Corrosion
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    Chapter 16 Helicopter Structural Integrity Program Of Polish Mi-24 Hind Helicopters
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    Chapter 17 Airframe Life Extension By Optimised Shape Reworking — Overview Of Dsto Developments
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    Chapter 18 Evaluation, Modification And Damage Tolerance Of An In-Service Aircraft Critical Area
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    Chapter 19 Procedures For Aircraft Structural Teardown Analysis: Development Of A Best Practices Handbook
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    Chapter 20 Fatigue Lifetime Improvement Of Arrestment Hook Shanks By Application Of Laser Peening
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    Chapter 21 Design and Testing of Advanced Composite Load Introduction Structure for Aircraft High Lift Devices
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    Chapter 22 Hybrid Structure Solution for the A400M Wing Attachment Frames
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    Chapter 23 Control of Crack Growth Rates and Crack Trajectories for Enhanced Fail Safety and Damage Tolerance in Welded Aircraft Structures
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    Chapter 24 Durability and Damage Tolerance of Bonded Repairs to Metallic Fuselage Structure
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    Chapter 25 Investigation on the Design of Bonded Structures for Increased Damage Tolerance
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    Chapter 26 An Experimental Investigation on the Fatigue Performance of Riveted Lap Joints
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    Chapter 27 Improving the Fatigue Life of Aeronautical Single-Lap Bolted Joints Thanks to the Hybrid (Bolted/Bonded) Joining Technology
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    Chapter 28 An Experimental Approach to Investigate Detailed Failure Mechanisms in Fibre Metal Laminates
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    Chapter 29 Experimental Determination of Energy Release Rate of Cfrp Structures by Means of Transverse Crack Tension Tests
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    Chapter 30 Central Material Concept: Towards Aircraft Wing Structure Insensitive to Fatigue
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    Chapter 31 Practical Applications of Improvements in Fml Crack Bridging Theory
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    Chapter 32 Simulation of the Stress Distribution on Fuselage Structures for the Pre- and Post Analyses of Curved Panel Tests
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    Chapter 33 Low Cycle Lifetime Prediction of Al2024 Alloy
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    Chapter 34 Fatigue and Damage Tolerance Aspects of Metal Laminates
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    Chapter 35 Arall and Glare Fml's: Three Decades of Bridging the Gap Between Theory and Operational Practice
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    Chapter 36 Detailed Strain Field Analyses Of Fatigue Cracks In Friction Stir Welded Joints
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    Chapter 37 A Study of Interaction and Coalescence of Micro Surface Fatigue Cracks in Aluminium 7050
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    Chapter 38 Fracture Behaviour of Skin Materials of Civil Airplane Structures
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    Chapter 39 Fatigue Life Prediction of Small Notched Ti-6Al-4V Based on The Theory of Critical Distance
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    Chapter 40 A Case Study of Multiple-Site Fatigue Crack Growth in the F-18 Hornet Bulkhead
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    Chapter 41 Experimental And Theoretical Comparison Of Some Multiaxial Fatigue Design Criteria In The Context Of Life Assessment Of Rotating Parts In Turboengines
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    Chapter 42 A Contribution Of Environmental Investigations For Glare Riveted Joint Sizing
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    Chapter 43 Advances In Crack Growth Modelling Of 3D Aircraft Structures
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    Chapter 44 Development Of Advanced Risk Assessment Methodologies For Aircraft Structures Containing Msd/Med
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    Chapter 45 Crack Growthin Fibre Metal Laminates Under Variable Amplitude Loading
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    Chapter 46 Effect Of Residual Stresses From Shot Peening On Fatigue Strength And Threshold To Crack Propagation Of Al 7475 Alloy Components
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    Chapter 47 Experimental Validation Of Stress Intensity Factor Solutions For The Pin Loaded Lug
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    Chapter 48 Properties Of Fatigue Crack Propagation In Friction Stir Welded 2024-T3 Aluminum Alloy
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    Chapter 49 Fatigue Crack Growth In Thick Plate 7050 Aluminum
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    Chapter 50 Fatigue Life Evaluation On Tension Type Fitting
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    Chapter 51 Accelerated Fatigue Testing on Hydraulic Shaker
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    Chapter 52 Methods for Fem Analysis of Riveted Joints of Thin-Walled Aircraft Structures Within the Imperja Project
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    Chapter 53 On the Crack Growth Behavior Under Simple Compressive Loads of 2024-T3 Aluminium Alloy
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    Chapter 54 An Analytical Model for Load Transfer in a Mechanically Fastened, Double-Lap Joint
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    Chapter 55 Simulation of Fatigue Crack Growth in the High Speed Machined Panel Under the Constant Amplitude and Spectrum Loading
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    Chapter 56 Bonded Composite Patch to Repair Metallic Structures: Disbond Propagation Testing and Modelling
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    Chapter 57 Three Diminsional Crack Growth Prediction
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    Chapter 58 Hybrid Structures for Concentrated Load Transmission in Fibre Composites: Initial Experiments
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    Chapter 59 Pilatus Pc-21 – A Damage Tolerant Aircraft
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    Chapter 60 Introduction to Service of an Artificial Neural Network Based Fatigue Monitoring System
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    Chapter 61 Towards Automated Flight-Maneuver-Specific Fatigue Analysis
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    Chapter 62 Service History Analysis and Teardown Evidence — Key Elements for Structural Usage Monitoring of an Ageing Fleet
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    Chapter 63 Development of Fatigue Life Monitoring of Rmaf Fighter Airplanes
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    Chapter 64 Research and Development of Impact Damage Detection System for Airframe Structures Using Optical Fiber Sensors
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    Chapter 65 Load Factor (Nz) / Roll Rate: First Comparisons Between Design and in-Flight Recorded Data on Eurofighter Typhoon Italian Fleet
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    Chapter 66 Development of a Structural Health Monitoring System to Evaluate De-Bonding in Composite Adhesive Structures
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    Chapter 67 Olm: A Hands-on Approach
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    Chapter 68 F-35 Joint Strike Fighter Structural Prognosis and Health Management an Overview
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    Chapter 69 Bonded Repair for Fuselage Damage: an Overall Benefit to Commercial Aviation
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    Chapter 70 Fatigue & Damage Tolerance of Hybrid Materials & Structures – Some Myths, Facts & Fairytales
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    Chapter 71 High Cycle Fatigue of Laser Beam Deposited Ti-6Al-4V and Inconel 718
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    Chapter 72 The Variable Expansion Process — a New Cost Efficient Method for Cold Working Fastener Holes in Aluminium Aircraft Structures
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    Chapter 73 Stress Measurements With X-Ray Diffractometry on Aluminum Alloys. Determination of the Most Optimized Parameters of the Measurement
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    Chapter 74 Delamination Growth at Interfaces in Hybrid Materials and Structures Under Various Opening Modes
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    Chapter 75 Developments in Metal Bonding
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    Chapter 76 On Separating the Effect of Corrosion on Inter-Lamellar Fatigue of Thin Sheet Aa7079-T6
Overall attention for this book and its chapters
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Title
ICAF 2009, Bridging the Gap between Theory and Operational Practice
Published by
Springer Netherlands, May 2009
DOI 10.1007/978-90-481-2746-7
ISBNs
978-9-04-812745-0, 978-9-04-812746-7
Editors

Bos, M. J.

Mendeley readers

Mendeley readers

The data shown below were compiled from readership statistics for 39 Mendeley readers of this research output. Click here to see the associated Mendeley record.

Geographical breakdown

Country Count As %
Spain 1 3%
Unknown 38 97%

Demographic breakdown

Readers by professional status Count As %
Student > Ph. D. Student 10 26%
Student > Doctoral Student 4 10%
Student > Bachelor 3 8%
Student > Master 3 8%
Researcher 3 8%
Other 5 13%
Unknown 11 28%
Readers by discipline Count As %
Engineering 14 36%
Materials Science 9 23%
Business, Management and Accounting 1 3%
Agricultural and Biological Sciences 1 3%
Unknown 14 36%