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ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives

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Cover of 'ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives'

Table of Contents

  1. Altmetric Badge
    Book Overview
  2. Altmetric Badge
    Chapter 1 Fleet Recovery and Life Extension – Some Lessons Learned
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    Chapter 2 Sticks and Stones
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    Chapter 3 Analysis of Requirements on Fatigue and Damage Tolerance for Civil Transport Airplanes
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    Chapter 4 Material Selection and Detailed Design – Requirements and Responsibilities of an Accredited and Qualified Test Laboratory
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    Chapter 5 Bombardier Aerospace FSW Demonstrator
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    Chapter 6 Evaluation of Fatigue Crack Growth Behavior in FSW Joint by Experiment, Analysis and Elasto-Plastic FEM
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    Chapter 7 Recent Development on Bonded Structures
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    Chapter 8 Recent Advancements in Thin-Walled Hybrid Structural Technologies for Damage Tolerant Aircraft Fuselage Applications
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    Chapter 9 Fatigue Life Assessment for Composite Structure
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    Chapter 10 Potential of CFRP Used for Light Weight Structures: Some Experimental Results
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    Chapter 11 An Implementation of an Accelerated Testing Methodology to Obtain Static, Creep and Fatigue Master Curves of a T300/913 Unidirectional Composite Material
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    Chapter 12 Improvement of Vibration Damping and Flexural Fatigue Property Incorporating Nanoclay into Glass/Epoxy Composite
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    Chapter 13 Formation of a Metal Coating by Means of Friction Stir Processing
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    Chapter 14 Influence of the Carbon Nanotube Type, Loading and Chemical Functionalization on the Fatigue Resistance of Aluminum Lap Joints
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    Chapter 15 Fatigue Damage Behavior of Glass/Epoxy Composites Using Carbon Nanotubes as Sensors
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    Chapter 16 DSTO – NLR Collaborative Programme on Fatigue Properties of β -Annealed Ti-6Al-4V: Preliminary Results
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    Chapter 17 Damage Tolerance Demonstration of Flange Joint for Aircraft Engine Composite Fan Case
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    Chapter 18 The Formation/Nucleation of Fatigue Cracks in Aircraft Structural Materials
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    Chapter 19 Modelling of Continuing Damage for Damage Tolerance Analysis
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    Chapter 20 The Critical Importance of Correctly Characterising Fatigue Crack Growth Rates in the Threshold Regime
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    Chapter 21 The Relationships between Crack Closure, Specimen Compliance and ‘Effective’ Fatigue Crack Growth Rate
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    Chapter 22 Experimental and Numerical Study of Stress and Strain Field around the Rivet
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    Chapter 23 Fatigue Analyses of Riveted Lap-Splice Joints in a Narrow-Body Aircraft
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    Chapter 24 Crack Growth Rate Curves: Which Part Dominates Life Prediction and When?
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    Chapter 25 Critical Distance for Fatigue Life Prediction in Aerospace Materials
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    Chapter 26 A Unified Variable-Amplitude Model for Crack Initiation and Crack Propagation
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    Chapter 27 Development of an Efficient Methodology and Tool to Determine Stress Intensity Correction Factors for Complex Aircraft Structures
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    Chapter 28 Improved SIF Calculation in Riveted Panel Type Structures Using Numerical Simulation
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    Chapter 29 An 1D-Beam Approach for Both Stress Analysis and Fatigue Life Prediction of Bonded Joints
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    Chapter 30 Cyclic Stress-Strain and Strain-Life Properties of Aerospace Metallic Materials
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    Chapter 31 Crack Propagation Calculation for Aluminium Aircraft Structures Considering the Influence of Load Sequences
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    Chapter 32 Analysis of Fatigue Crack Growth under Random Load Sequences Derived from Military In-flight Load Data
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    Chapter 33 Statistical Analysis of Fatigue Crack Growth Based on the Unigrow Model
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    Chapter 34 Fatigue Life Estimation of Structures Subjected to Vibratory Loading
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    Chapter 35 A Structural Defect Expansion Model Based on Physical Correlation
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    Chapter 36 Link between Flight Maneuvers and Fatigue
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    Chapter 37 Health and Usage Monitoring of Unmanned Aerial Vehicles Using Fiber-Optic Sensors
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    Chapter 38 Airframe Loads and Usage Monitoring of the CH-47D “Chinook” Helicopter of the Royal Netherlands Air Force
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    Chapter 39 Damage Detection System for Automated Hot Spot Monitoring Based on Different Technologies Used in Component Testing for Shot Peening Validation
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    Chapter 40 Memorization and Detection of an Arrested Crack in Foam-Core Sandwich Structures Using Embedded Metal Wires and Fiber-Optic Sensors
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    Chapter 41 Structural Load Monitoring Systems for Military Aircraft in the Polish Armed Forces with Examples of Selected Activities
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    Chapter 42 A320 ESG Full Scale Fatigue Test - Lessons Learned
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    Chapter 43 New Connection Strap Concepts for A320 Wheel Well Area Tested during the Airbus A320 Extended Service Goal Full Scale Fatigue Test
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    Chapter 44 Full-Scale Static and Fatigue Testing of Composite Fuselage Section
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    Chapter 45 Durability and Damage Tolerance Evaluation of VaRTM Composite Wing Structure
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    Chapter 46 Development of Load Spectrum for Full Scale Fatigue Test of a Trainer Aircraft
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    Chapter 47 ATR Life Extension Project
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    Chapter 48 Benefits of Using a Risk Process in Asip – The CF-18 Experience
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    Chapter 49 Integrated Probabilistic Analysis of Damage Tolerance and Risk for Airframe Structural Locations
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    Chapter 50 Aircraft Joints and Corrosion Control
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    Chapter 51 A Case Study of Nose Landing Gear Failure Caused by Fatigue
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    Chapter 52 Test Method for Determining the Effect of Chromate Primers on Fatigue Crack Growth
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    Chapter 53 Life Extension: Fatigue Lifetime Updating of the French Xingu Fleet
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    Chapter 54 Fatigue Life of Cold Expanded Fastener Holes at Short Edge Margins
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    Chapter 55 Environmentally Assisted Cracking in Advanced Aerospace Aluminums
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    Chapter 56 An Overview of Fretting Aspects Relating to Aero-Engine Dovetail Attachment
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    Chapter 57 Fatigue Analysis of the Compressor Blades with V- Notches
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    Chapter 58 Fatigue and Residual Strength Performance of Bonded Repairs to Metallic Fuselage
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    Chapter 59 Life Extension Techniques for Aircraft Structures – Extending Durability and Promoting Damage Tolerance through Bonded Crack Retarders
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    Chapter 60 Damage Tolerance of Adhesive Bonded Stiffened Panels: Experimental and Analytical Investigation of the Fatigue Crack Propagation Underneath the Stringers
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    Chapter 61 Development of a New Fiber Metal Laminate Variant Optimized for Cold Expansion and Riveting of Holes
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    Chapter 62 Applying the Damage Tolerance Approach to Expanded Bushing and Rivetless Nut Plate Installations
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    Chapter 63 Fatigue Life Improvement of Metallic Aerospace Structures via Crenellations
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    Chapter 64 Fatigue Life Improvement Using In-situ Robotic Processes
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    Chapter 65 Investigations into the Fatigue Enhancement Provided by the Hole Cold Expansion Process Using Accurate 3D FEA Simulations and Fatigue Testing
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    Chapter 66 Characterisation of Fatigue and Crack Propagation in Laser Shock Peened Open Hole 7075-T73 Aluminium Specimens
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    Chapter 67 Damage Tolerance of Titanium Alloy Rotorcraft Components: Advantages and Challenges
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    Chapter 68 NH90 Qualification According to Damage Tolerance
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    Chapter 69 Damage Tolerance for Composite Parts
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    Chapter 70 Towards Weight Savings for Damage Tolerant Masts and Driveshafts
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    Chapter 71 Challenges in Damage Tolerance Approach for Dynamic Loaded Rotorcraft Components – From Risk Assessment to Optimal Inspection Planning
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    Chapter 72 Improvements in Fatigue Evaluations of Helicopter Transmissions
Overall attention for this book and its chapters
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Title
ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives
Published by
Springer Science & Business Media, May 2011
DOI 10.1007/978-94-007-1664-3
ISBNs
978-9-40-071664-3, 978-9-40-071663-6
Editors

Komorowski, Jerzy, Komorowski, Jerzy

Mendeley readers

Mendeley readers

The data shown below were compiled from readership statistics for 24 Mendeley readers of this research output. Click here to see the associated Mendeley record.

Geographical breakdown

Country Count As %
Unknown 24 100%

Demographic breakdown

Readers by professional status Count As %
Student > Ph. D. Student 7 29%
Student > Master 6 25%
Student > Doctoral Student 5 21%
Student > Bachelor 2 8%
Professor > Associate Professor 2 8%
Other 1 4%
Unknown 1 4%
Readers by discipline Count As %
Engineering 16 67%
Materials Science 3 13%
Agricultural and Biological Sciences 1 4%
Physics and Astronomy 1 4%
Unknown 3 13%