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ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives

Proceedings of the 26th Symposium of the International Committee on Aeronautical Fatigue, Montreal, Canada, 1-3 June 2011

  • Conference proceedings
  • © 2011

Overview

Editors:
  1. Jerzy Komorowski

    1. National Research Council Canada, Institute for Aerospace Research, Ottawa, Canada

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  • ICAF Symposium has a history of being a location for presentation of significant papers on aeronautical fatigue design practices
  • Bi-annual update on the state of the art for aeronautical design and engineering
  • Wide international participation of senior industrial, government and research leaders

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About this book

Proceedings of the 26th Symposium of the International Committee on Aeronautical Fatigue are a widely referenced summary of advances in aeronautical design against fatigue. This is a bi-annual event and the proceedings have been published in book form for over 35 years.

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Table of contents (72 papers)

  1. Structural Health and Structural Loads Monitoring

    1. Memorization and Detection of an Arrested Crack in Foam-Core Sandwich Structures Using Embedded Metal Wires and Fiber-Optic Sensors

      • Shu Minakuchi, Nobuo Takeda, Yasuo Hirose
      Pages 507-517

    2. Structural Load Monitoring Systems for Military Aircraft in the Polish Armed Forces with Examples of Selected Activities

      • M. Kurdelski, A. Leski, S. Klimaszewski, M. Stefaniuk
      Pages 519-527

  2. Full Scale Fatigue Testing of Aircraft and Aircraft Components

    1. A320 ESG Full Scale Fatigue Test - Lessons Learned

      • G. Hilfer, N. Rößler, C. Peters, C. Herrmann
      Pages 529-537

    2. New Connection Strap Concepts for A320 Wheel Well Area Tested during the Airbus A320 Extended Service Goal Full Scale Fatigue Test

      • Nikola Cenic, Bernd Zapf, Till Haberle
      Pages 539-549

    3. Full-Scale Static and Fatigue Testing of Composite Fuselage Section

      • Rushabh Kothari
      Pages 551-560

    4. Durability and Damage Tolerance Evaluation of VaRTM Composite Wing Structure

      • Yuichiro Aoki, Yoshiyasu Hirano, Sunao Sugimoto, Yutaka Iwahori, Yosuke Nagao, Takeshi Ohnuki
      Pages 561-572

    5. Development of Load Spectrum for Full Scale Fatigue Test of a Trainer Aircraft

      • Andrzej Leski, Piotr Reymer, Marcin Kurdelski
      Pages 573-584

  3. Inservice Experience, Life Extension and Management of Ageing Fleets

    1. ATR Life Extension Project

      • Maurizio Cajani, Roberto Ciotola, Jérémy David, Jaco Salvi
      Pages 585-600

    2. Benefits of Using a Risk Process in Asip – The CF-18 Experience

      • Yves Beauvais
      Pages 601-613

    3. Integrated Probabilistic Analysis of Damage Tolerance and Risk for Airframe Structural Locations

      • W. Hu, R. F. Torregosa
      Pages 615-624

    4. Aircraft Joints and Corrosion Control

      • Ung Hing Tiong, Graham Clark
      Pages 625-634

    5. A Case Study of Nose Landing Gear Failure Caused by Fatigue

      • V. Y. Guertsman
      Pages 635-644

    6. Test Method for Determining the Effect of Chromate Primers on Fatigue Crack Growth

      • Yongwon Lee, Sarah E. Galyon Dorman, Matthew J. Hammond
      Pages 645-654

    7. Life Extension: Fatigue Lifetime Updating of the French Xingu Fleet

      • P. Madelpech, D. Théret, M. Fressinet, J. Despujols, B. André
      Pages 655-669

    8. Fatigue Life of Cold Expanded Fastener Holes at Short Edge Margins

      • G. M. Vallières, D. L. DuQuesnay
      Pages 671-684

    9. Environmentally Assisted Cracking in Advanced Aerospace Aluminums

      • E. M. Arnold, J. J. Schubbe, P. J. Moran, R. Bayles
      Pages 685-696

    10. An Overview of Fretting Aspects Relating to Aero-Engine Dovetail Attachment

      • Raghu V. Prakash, K. Anandavel, P. Balasubramani
      Pages 697-720

    11. Fatigue Analysis of the Compressor Blades with V- Notches

      • Lucjan Witek
      Pages 721-734

  4. Fatigue Life Enhancement Methods and Repair Solutions

    1. Fatigue and Residual Strength Performance of Bonded Repairs to Metallic Fuselage

      • John G. Bakuckas Jr., Bud Westerman
      Pages 735-752

    2. Life Extension Techniques for Aircraft Structures – Extending Durability and Promoting Damage Tolerance through Bonded Crack Retarders

      • P. E. Irving, X. Zhang, J. Doucet, D. Figueroa-Gordon, M. Boscolo, M. Heinimann et al.
      Pages 753-770
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Editors and Affiliations

  • National Research Council Canada, Institute for Aerospace Research, Ottawa, Canada

    Jerzy Komorowski

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