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ICAF 2009, Bridging the Gap between Theory and Operational Practice

Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, The Netherlands, 27-29 May 2009

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  • © 2009
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Overview

Editors:
  1. M. J. Bos

    1. National Aerospace Laboratory NLR, Amsterdam, The Netherlands

  • Coverage of all areas related to aeronautical fatigue and aircraft structural integrity

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About this book

The 31st Conference and the 25th Symposium of the International Committee on Aeronautical Fatigue will be hosted in Rotterdam, The Netherlands, by the National Aerospace Laboratory NLR, under the auspices of the Netherlands Association of Aeronautical Engineers NVvL, the Technical University of Delft and Stork Fokker AESP B.V.

These Proceedings will consist of reviews of aeronautical fatigue activities presented by the national delegates of the 14 member nations of ICAF. It will also contain specialist papers presented by international authors with design, manufacturing, airworthiness regulations, operations and research backgrounds. The papers will be based on the theme “Bridging the gap between theory and operational practice”.

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Table of contents (76 papers)

  1. Front Matter

    Pages i-xviii
    Download chapter PDF

  2. Full-Scale Fatigue Testing of Aircraft and Aircraft Structural Components

    1. A Test Concept For Future Aircraft Fuselage Panels

      • R. Best, Th. Fleischer, M. Götze, M. Sachse, M. Semsch
      Pages 3-14

    2. Marker Loads for Quantitative Fractography of Fatigue Cracks in Aerospace Alloys

      • S. A. Barter, L. Molent, R. J. H. Wanhill
      Pages 15-54

    3. Substantiations of an Airborne Composite Radome Mounted on an Aircraft Dome

      • I. Kressel, U. Ben-Simon, M. Elyahu, D. Peled, A. David, T. Nachshhon et al.
      Pages 55-58

  3. Airworthiness Considerations

    1. 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

      • Girindra K. Das, Matthew Miller
      Pages 61-71

    2. Damage Tolerance Philosophy for Bonded Aircraft Structures

      • C. D. Rans, R. C. Alderliesten
      Pages 73-90

    3. First Diamond

      • Steve Swift
      Pages 91-107

    4. Survey of Structural Repairs and Alterations in Transport Category Airplanes

      • Michel D. Bode, Walter Sippel, John G. Bakuckas
      Pages 109-121

    5. Enhanced Teardown of Ex-Service F/A-18A/B/C/D Centre Fuselages

      • L. Molent, B. Dixon, S. Barter, P. White, T. Mills, K. Maxfield et al.
      Pages 123-142

  4. NDI, Inspections and Maintenance

    1. Glare Teardowns From the Megaliner Barrel (Mlb) Fatigue Test

      • R. J. H. Wanhill, D. J. Platenkamp, T. Hattenberg, A. F. Bosch, P. H. de Haan
      Pages 145-167

    2. 30 Years of Damage Tolerance – Have we Got it Right?

      • Robert G. Eastin, Jon B. Mowery
      Pages 169-186

    3. Compilation Of Damage Findings From Multiple Recent Teardown Analysis Programs

      • Gregory A. Shoales, Scott A. Fawaz, Molly R. Walters
      Pages 187-207

    4. Detection Of Arrested Crack For Foam Core Sandwich Structures Using Optical Fiber Sensors Embedded In A Crack Arrester

      • Shu Minakuchi, Ippei Yamauchi, Nobuo Takeda, Yasuo Hirose
      Pages 209-221

  5. Life Extension and Management of Ageing Fleets

    1. Concept Of The New A320 Fatigue Test

      • N. Rößler, C. Peters, O. Tusch, G. Hilfer, C. Herrmann
      Pages 225-236

    2. The Use Of Composite Material Strips To Extend The Damage-Tolerance Life Of Integrally Stiffened Aluminum Panels

      • A. Brot, Y. Peleg-Wolfin, I. Kressel, Z. Yosef
      Pages 237-244

    3. Structural Integrity Of A Wing Upper Skin With Exfoliation Corrosion

      • Andreas Uebersax, Cyril Huber, Guillaume Renaud, Min Liao
      Pages 245-261

    4. Helicopter Structural Integrity Program Of Polish Mi-24 Hind Helicopters

      • Sławomir Klimaszewski, Andrzej Leski, Krzysztof Dragan, Marcin Kurdelski, Mirosław Wrona
      Pages 263-277

    5. Airframe Life Extension By Optimised Shape Reworking — Overview Of Dsto Developments

      • M. Heller, M. Burchill, R. Wescott, W. Waldman, R. Kaye, R. Evans et al.
      Pages 279-299

    6. Evaluation, Modification And Damage Tolerance Of An In-Service Aircraft Critical Area

      • R. S. Rutledge, D. S. Backman, R. J. Hiscocks
      Pages 301-327

    7. Procedures For Aircraft Structural Teardown Analysis: Development Of A Best Practices Handbook

      • Gregory Shoales
      Pages 330-353
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Editors and Affiliations

  • National Aerospace Laboratory NLR, Amsterdam, The Netherlands

    M. J. Bos

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Bibliographic Information

  • Book Title: ICAF 2009, Bridging the Gap between Theory and Operational Practice

  • Book Subtitle: Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, The Netherlands, 27-29 May 2009

  • Editors: M. J. Bos

  • DOI: https://doi.org/10.1007/978-90-481-2746-7

  • Publisher: Springer Dordrecht

  • eBook Packages: Engineering, Engineering (R0), Springer Nature Proceedings excluding Computer Science

  • Copyright Information: Springer Science+Business Media B.V. 2009

  • Hardcover ISBN: 978-90-481-2745-0Published: 26 May 2009

  • eBook ISBN: 978-90-481-2746-7Published: 24 May 2009

  • Edition Number: 1

  • Number of Pages: XVIII, 1370

  • Topics: Automotive Engineering, Mechanical Engineering, Engineering Design

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