Icaf 2009, Bridging The Gap Between Theory And Operational Practice: Proceedings of the 25th Symposium of the International Committee on Aeronautical  by M. BosIcaf 2009, Bridging The Gap Between Theory And Operational Practice: Proceedings of the 25th Symposium of the International Committee on Aeronautical  by M. Bos

Icaf 2009, Bridging The Gap Between Theory And Operational Practice: Proceedings of the 25th…

EditorM. Bos

Hardcover | May 26, 2009

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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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Title:Icaf 2009, Bridging The Gap Between Theory And Operational Practice: Proceedings of the 25th…Format:HardcoverDimensions:1388 pages, 9.25 × 6.1 × 0.98 inPublished:May 26, 2009Publisher:Springer NetherlandsLanguage:English

The following ISBNs are associated with this title:

ISBN - 10:9048127459

ISBN - 13:9789048127450

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Table of Contents

Preface; ICAF General Secretary & National Delegates ; FULL-SCALE FATIGUE TESTING OF AIRCRAFT AND AIRCRAFT STRUCTURAL COMPONENTS: A test concept for future aircraft fuselage panels, by R. Best, Th. Fleischer, M. Gotze, M Sachse and M Semsch ; Marker loads for quantitative fractography of fatigue cracks in aerospace alloys, by S.A. Barter, L. Molent and RJ.H. Wanhill; Substantiations of an airborne composite radome mounted on an aircraft dome, by I. Kressel, U. Ben-Simon, M Elyahu, D. Peled, A. David, T. Nachshhon, Y. Gary, M Interator, G. Ghilai and A. Simon ; AIRWORTHINESS CONSIDERATIONS: 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, by Girindra K. Das and Matthew Miller ; Damage tolerance philosophy for bonded aircraft structures, by C.D. Runs and R. C. Alderliesten ; First diamond: 'Damage tolerance' for the structural honeymoon, by Steve Swiji ; Survey of structural repairs and alterations in transport category airplanes, by Michel D. Bode, Walter Sippel and John G. Bakuckas ; Enhanced teardown of ex-service FIA- 18A/B/C/D centre fuselages, by L. Molent, B. Dixon, S. Barter, P. White, T. Mills, K. MaxJield, G. Swanton and B. Main ; NDI, INSPECTIONS AND MAINTENANCE: Glare teardowns from the MegaLiner Barrel (MLB) fatigue test, by R.J.H. Wanhill, D.J. Platenkamp, T. Hattenberg, A.F. Bosch and P.H. de Haan ; 30 Years of damage tolerance - Have we got it right?, by Robert G. Eastin and Jon B. Mowery ; Compilation of damage findings fiom multiple recent teardown analysis programs, by Gregory A. Shoales, Scott A. Fawaz and Molly R. Walters ; Detection of arrested crack for foam core sandwich structures using optical fiber sensors embedded in a crack arrester, by Shu Minakuchi, Ippei Yamauchi, Nobuo Takeda and Yasuo Hirose ; LIFE EXTENSION AND MANAGEMENT OF AGEING FLEETS: Concept of the new A320 fatigue test, by N. Rojler, C. Peters, 0. Tusch, G. Hilfer and C. Herrmann; The use of composite material strips to extend the damage-tolerance life of integrally stiffened aluminium panels, by A. Brot, Y. Peleg- WolJin,I . Kressel and Z. Yosef ; Structural integrity of a wing upper skin with exfoliation corrosion, by Andreas Uebersax, Cyril Huber, Guillaume Renaud and Min Liao ; Helicopter structural integrity program of Polish Mi-24 Hind helicopters, by Slawomir Klirnaszewski, Atldrzej Leski, Krzysztof Dragan, Marcin Kurdelski and Miroslaw Wrona ; Airframe life extension by optimised shape reworking - Overview of DSTO developments, by M. Heller, M. Burchill, R. Westcott, K Waldman, R. Kaye, R. Evans and M. McDonald ; Evaluation, modification and damage tolerance of an in-service aircraft critical area, by R.S. Rutledge, D.S. Backman and R.J. Hiscocks ; Procedures for aircraft structural teardown analysis: Development of a best practices handbook, by Gregory A. Shoales; Fatigue lifetime improvement of arrestment hook shanks by application of laser peening, by Mike Leap, Jon Rankin, Jim Harrison, Serena Marley, Lloyd Hackel and Joe Nemeth; ADVANCED MATERIALS AND INNOVATIVE STRUCTURALCONCEPTS: Design and testing of advanced composite load introduction structure foraircraft high lift devices, by Tamas Havar and Eckart Stuible ; Hybrid structure solution for the A400M wing attachment frames, by Matthijs Plokker, Derk Daverschot and Thomas Beumler ; Control of crack growth rates and crack trajectories for enhanced fail safety and damage tolerance in welded aircraft structures, by Phil Irving, Yu E Ma, Xiang Zhang, Guido Sewetti, Stewart Williams, Gary Moore, Jorge dos Santos and Marco Pacchione ; Durability and damage tolerance of bonded repairs to metallic fuselage Structure, by John G. Bakuckas, Jr., Keith McIver and Ching Hsu ; Investigation on the design of bonded structures for increased damage Tolerance, by Ivan Meneghin, Marco Pacchione and Pascal Venneer ; An experimental investigation on the fatigue performance of riveted lap Joints, by M. Skorupa, A. Skorupa, T. Machniewicz andA. Korbel ; Improving the fatigue life of aeronautical single lap bolted joints thanks to the hybrid (boltedhonded) joining technology, by E. Paroissien, C. T. Hoang Ngoc, H. Bhugaloo and D. Ducher ; An experimental approach to investigate detailed failure mechanisms in fibre metal laminates, by Riccardo Rodi, Rend Alderliesten and Rinze Benedictus ; Experimental determination of energy release rate of CFRP structures by means of transverse crack tension tests, by Ll. Llopart Prieto, G. Spenninger and H. Wagner ; Central material concept: towards aircraft wing structure insensitive to Fatigue, by Mohamed A.A. Attia ; Practical applications of improvements in FML. crack bridging theory, by Greg Wilson, Renk Alderliesten, Riccardo Rodi and H.J.K. Lemmen; Simulation of the stress distribution on fuselage structures for the preand post analysis of curved panel tests, by Matthias Ziegenhom, Frank Schulze, Holger Spar, Karsten Wenke and Thomas Fleischer ; Low cycle lifetime prediction of AL2024 alloy, by A. Vyshnevskyy, S. Khan and J. Mosler ; Fatigue and damage tolerance aspects of metal laminates, by J. Sinke and S.A. H. Johansson ; Arall and Glare FML's: Three decades of bridging the gap between theory and operational practice, by Cees van Hengel and Peter Kortbeek ; FATIGUE CRACK GROWTH AND LIFE PREDICTION METHODS: Detailed strain field analyses of fatigue cracks in fiiction stir welded Joints, by H.J.K. Lemmen, R. C. Alderliesten and R. Benedictus ; A study of interaction and coalescence of micro surface fatigue cracks in aluminium 7050, by W. Hu, Q. Liu andS. Barter; Fracture behaviour of skin materials of civil airplane structures, by Boris Nesterenko, Grirory I. Nesterenko and Valentin N. Basov ; Fatigue life prediction of small notched TI-6AL-4V based on the theory of critical distance, by Yoichi Yamashita, Masaharu Shinozaki, Hiroshi Kuroki and Yusuke Ueda ; A case study of multiple-site fatigue crack growth in the F-18 Hornet Bulkhead, by B. Andersson, A.F. Blom, U. Falk, G.S. Wang, K. Koski, A. Siljander, J. Linna, A. Miettinen, K. Vaaraniemi and R. Lahtinen; Experimental and theoretical comparison of some multiaxial fatigue design criteria in the context of life assessment of rotating parts in turboengines, by V. Bonnand, J.L. Chaboche, H. Cherouali, P. Gomez, P. Kanoutk, D. Pacou, P. Paulmier, E. Ostoja-Kuczynski and F. Vogel; A contribution of environmental investigations for Glare riveted joint sizing, by Thomas Beumler, Bob Borgonje and Jos Sinke ; Advances in crack growth modelling of 3D aircraft structures, by S. C. Mellings, J. M W. Baynham and R.A. Adey; Development of advanced risk assessment methodologies for aircraft structures containing MSD/MED, by Min Liao, Yan Bombardier, Guillaume Renaud, Nick Bellinger and Terence Cheung ; Crack growth in fiber metal laminates under variable amplitude loading, by S. U. Khan, R. C. Alderliesten and R. Benedictus ; Effect of residual stresses from shot peening on fatigue strength and threshold to crack propagation of AL 7475 alloy components, by G. Ratti, U. Mariani, M Giglio and M. Cuagliano ; Experimental validation of stress intensity factor solutions for the pin loaded lug, by D.R. Child, N.J. Moyle and A.F. Grandt ; Properties of fatigue crack propagation in friction stir welded 2024-T3 aluminum alloy, by T. Okada, K. Kuwayama,,S. Fujita, M. Asakawa, T. Nakamura and S. Machida; Fatigue crack growth in thick plate 7050 aluminum, by Joel Schubbe ; Fatigue life evaluation on tension type fitting, by Nicolas Barta and Marie Masst ; Accelerated fatigue testing on hydraulic shaker, by M. Fressinet. M Panis and C. Bordes ; Methods for FEM analysis of riveted joints of thin-walled aircraft structures within the Imperja project, by Jerzy Kaniowski, Wojciech Wronicz, Jerzy Jachimowicz and E. Szymczyk ; On the crack growth behaviour under simple compressive loads of 2024-T3 aluminium alloy, by M Krkoika, R. C. Alderliesten and R. Benedictus ; An analytical model for load transfer in a mechanically fastened, double-lap joint, by Ligieja Paletti, Calvin Rans and Rinze Benedictus ; Simulation of fatigue crack growth in the high speed machined panel under the constant amplitude and spectrum loading, by Petr Augustin ; Bonded composite patch to repair metallic structures: Disbond propagation testing and modelling, by P. Madelpech, S. Juaneda and M. Pradels ; Three dimensional crack growth prediction, by Sarah E. Galyon, Saravanan R. Arunachalam, James Greer, Matthew Hammond and Scott A. Fawaz ; Hybrid structures for concentrated load transmission in fibre composites: Initial experiments, by Pascal Vermeer, Rend Alderliesten and Rinze Benedictus ; STRUCTURAL HEALTH AND STRUCTURAL LOADS MONITORING: Pilatus PC-2 1 - A damage tolerant aircraft, by Lukas Schmid ; Introduction to service of an artificial neural network based fatigue monitoring system, by Steve Reed, Brian McCoubrey and Andy Mountfort ; Towards automated flight-maneuver-specific fatigue analysis, by Juha Jylha, Marja Ruotsalainen, Tuomo Salonen, Harri Janhunen, Tomi Viitanen,J uho Vihonen and Ari Visa ; Service history analysis and teardown evidence - Key elements for structural usage monitoring of an ageing fleet, by K.A. Lucas and MJ. DufJield ; Development of fatigue life monitoring of RMAF fighter airplanes, by Wahyu Kuntjoro, M. Suhaimi Ashari, M Yazid Ahmad and Assanah M wdin ; Research and development of impact damage detection system for akfiame structures using optical fiber sensors; Hiroaki Tsutsui, Noriyoshi Hirano, Junichi Kimoto, Takahiko Akatsuka, HiroJirmi Sashikuma, Nobuo Takeda and Naoyuki Tajima ; Load factors (NIZ) 1 roll rate: First comparisons between design and inflight recorded data on Eurofighter typhoon Italian fleet, by Tommaso Giacobbe and Fabio Sardo ; Development of a structural health monitoring system to evaluate debonding in composite adhesive structures, by Hideki Soejima, Noritsugu Nakamura, Toshimichi Ogisu, Hiroshi Wakai, Yoji Okabe, Nobuo Takeda and Yoshihiro Koshioka ; OLM: A hands-on approach, by Stephen Willis ; F-35 Joint strike fighter structural prognosis and health management: An Overview, by Timothy Fallon, Devinder Mahal and Iain Hebden ; FATIGUE LIFE ENHANCEMENT METHODS AND REPAIR SOLUTIONS: Bonded repair for fuselage damage: An overall benefit to commercial Aviation, by D. Fuflari, H.J.M Woerden, R. Benedictus and A. Kwakemaak ; Fatigue & damage tolerance of hybrid materials & structures - Some myths, facts & fairytales, by R. C. Alderliesten ; High cycle fatigue of laser beam deposited Ti-6A1-4V and inconel 718, by E. Amsterdam and G.A. Kool ; The variable expansion process - A new cost efficient method for cold working fastener holes in aluminium aircraft structures, by Eggert D. Reese, Anthony L. Dowson and Timothy G.B. Jones ; Stress measurements with x-ray difiactometry on aluminium alloys. Determination of the most optimized parameters of the measurement, by Elibieta Gadaliriska, Jerzy Kaniowski and Andrzej Wojtas; Delamination growth at interfaces in hybrid materials and structures under various opening modes, by G. Delgrange, R. C. Alderliesten and R. Benedictus ; Developments in metal bonding, by Jarkko J. Aakkula , Kari Lumppio, Olli Saarela and Tapani Haikola; ENVIRONMENTAL EFFECTS: On separating the effect of corrosion on inter-lamellar fatigue on thin sheet AA7079-T6, by Sandeep R. Shah and S.A. Fawaz; Authors Index