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 (English)
- New search for: International Committee on Aeronautical Fatigue
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- New search for: Bos, Marcel J.
- New search for: International Committee on Aeronautical Fatigue
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2009
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ISBN:
- Conference Proceedings / Print
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Title: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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Additional title:Bridging the gap between theory and operational practice
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Contributors:
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Conference:ICAF 2009 ; 25 ; 2009 ; Rotterdam
Symposium of the International Committee on Aeronautical Fatigue ; 25 ; 2009 ; Rotterdam -
Published in:ICAF-Doc. ; 2420
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Publisher:
- New search for: Springer
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Place of publication:Dordrecht [u.a.]
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Publication date:2009
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Size:XVIII, 1367 S
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Remarks:235 mm x 155 mm
Ill., graph. Darst -
ISBN:
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Type of media:Conference Proceedings
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Type of material:Print
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Language:English
- New search for: 629.13431 / 629.134/31
- Further information on Dewey Decimal Classification
- New search for: 51.32 / 55.50
- Further information on Basic classification
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Keywords:
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Classification:
DDC: 629.13431 / 629.134/31 BKL: 51.32 Werkstoffmechanik / 55.50 Luftfahrzeugtechnik -
Source:
Table of contents conference proceedings
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 3
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A test concept for future aircraft fuselage panelsBest, R. / Fleischer, T. / Gotze, M. / Sachse, M. / Semsch, M. et al. | 2009
- 15
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Marker loads for quantitative fractography of fatigue cracks in aerospace alloysBarter, S.A. / Molent, L. / Wanhill, R.J.H. et al. | 2009
- 55
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Substantiations of an airborne composite radome mounted on an aircraft domeKressel, I. / Ben-Simon, U. / Elyahu, M. / Peled, D. / David, A. / Nachshhon, T. / Gary, Y. / Interator, M. / Ghilai, G. / Simon, A. et al. | 2009
- 61
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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 regulationDas, G.K. / Miller, M. et al. | 2009
- 73
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Damage tolerance philosophy for bonded aircraft structuresRans, C.D. / Alderliesten, R.C. et al. | 2009
- 91
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First diamond: `Damage tolerance' for the structural honeymoonSwift, S. et al. | 2009
- 109
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Survey of structural repairs and alterations in transport category airplanesBode, M.D. / Sippel, W. / Bakuckas, J.G. et al. | 2009
- 123
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Enhanced teardown of ex-service F/A-18A/B/C/D centre fuselagesMolent, L. / Dixon, B. / Barter, S. / White, P. / Mills, T. / Maxfield, K. / Swanton, G. / Main, B. et al. | 2009
- 143
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Glare teardowns from the MegaLiner Barrel (MLB) fatigue testWanhill, R.J.H. / Platenkamp, D.J. / Hattenberg, T. / Bosch, A.F. / de Haan, P.H. et al. | 2009
- 169
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30 Years of damage tolerance - Have we got it right?Eastin, R.G. / Mowery, J.B. et al. | 2009
- 187
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Compilation of damage findings from multiple recent teardown analysis programsShoales, G.A. / Fawaz, S.A. / Walters, M.R. et al. | 2009
- 209
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Detection of arrested crack for foam core sandwich structures using optical fiber sensors embedded in a crack arresterMinakuchi, S. / Yamauchi, I. / Takeda, N. / Hirose, Y. et al. | 2009
- 225
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Concept of the new A320 fatigue testRossler, N. / Peters, C. / Tusch, O. / Hilfer, G. / Herrmann, C. et al. | 2009
- 237
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The use of composite material strips to extend the damage-tolerance life of integrally stiffened aluminium panelsBrot, A. / Peleg-Wolfin, Y. / Kressel, I. / Yosef, Z. et al. | 2009
- 245
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Structural integrity of a wing upper skin with exfoliation corrosionUebersax, A. / Huber, C. / Renaud, G. / Liao, M. et al. | 2009
- 263
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Helicopter structural integrity program of Polish Mi-24 Hind helicoptersKlimaszewski, S. / Leski, A. / Dragan, K. / Kurdelski, M. / Wrona, M. et al. | 2009
- 279
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Airframe life extension by optimised shape reworking - Overview of DSTO developmentsHeller, M. / Burchill, M. / Westcott, R. / Waldman, W. / Kaye, R. / Evans, R. / McDonald, M. et al. | 2009
- 301
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Evaluation, modification and damage tolerance of an in-service aircraft critical areaRutledge, R.S. / Backman, D.S. / Hiscocks, R.J. et al. | 2009
- 329
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Procedures for aircraft structural teardown analysis: Development of a best practices handbookShoales, G.A. et al. | 2009
- 355
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Fatigue lifetime improvement of arrestment hook shanks by application of laser peeningLeap, M. / Rankin, J. / Harrison, J. / Marley, S. / Hackel, L. / Nemeth, J. et al. | 2009
- 365
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Design and testing of advanced composite load introduction structure for aircraft high lift devicesHavar, T. / Stuible, E. et al. | 2009
- 375
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Hybrid structure solution for the A400M wing attachment framesPlokker, M. / Daverschot, D. / Beumler, T. et al. | 2009
- 387
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Control of crack growth rates and crack trajectories for enhanced fail safety and damage tolerance in welded aircraft structuresIrving, P. / Ma, Y.E. / Zhang, X. / Servetti, G. / Williams, S. / Moore, G. / dos Santos, J. / Pacchione, M. et al. | 2009
- 407
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Durability and damage tolerance of bonded repairs to metallic fuselage structureBakuckas, J.G. / McIver, K. / Hsu, C. et al. | 2009
- 427
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Investigation on the design of bonded structures for increased damage toleranceMeneghin, I. / Pacchione, M. / Vermeer, P. et al. | 2009
- 449
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An experimental investigation on the fatigue performance of riveted lap jointsSkorupa, M. / Skorupa, A. / Machniewicz, T. / Korbel, A. et al. | 2009
- 475
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Improving the fatigue life of aeronautical single lap bolted joints thanks to the hybrid (bolted/bonded) joining technologyParoissien, E. / Ngoc, C.T.H. / Bhugaloo, H. / Ducher, D. et al. | 2009
- 493
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An experimental approach to investigate detailed failure mechanisms in fibre metal laminatesRodi, R. / Alderliesten, R. / Benedictus, R. et al. | 2009
- 513
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Experimental determination of energy release rate of CRFP structures by means of transverse crack tension testsLlopart Prieto, L. / Spenninger, G. / Wagner, H. et al. | 2009
- 513
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Experimental determination of energy release rate of CFRP structures by means of transverse crack tension testsPrieto, L.L. / Spenninger, G. / Wagner, H. et al. | 2009
- 529
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Central material concept: towards aircraft wing structure insensitive to fatigueAttia, M.A.A. et al. | 2009
- 539
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Practical applications of improvements in FML crack bridging theoryWilson, G. / Alderliesten, R. / Rodi, R. / Lemmen, H.J.K. et al. | 2009
- 559
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Simulation of the stress distribution on fuselage structures for the pre- and post analyses of curved panel testsZiegenhorn, Matthias / Schulze, Frank / Sparr, Holger / Wenke, Karsten / Fleischer, Thomas et al. | 2009
- 559
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Simulation of the stress distribution on fuselage structures for the pre- and post analysis of curved panel testsZiegenhorn, M. / Schulze, F. / Sparr, H. / Wenke, K. / Fleischer, T. et al. | 2009
- 569
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Low cycle lifetime prediction of AL2024 alloyVyshnevskyy, A. / Khan, S. / Mosler, J. et al. | 2009
- 569
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Low cycle lifetime prediction of AL2O24 alloyVyshnevskyy, A. / Khan, S. / Mosler, J. et al. | 2009
- 585
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Fatigue and damage tolerance aspects of metal laminatesSinke, J. / Johansson, S.A.H. et al. | 2009
- 601
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Arall and Glare FML's: Three decades of bridging the gap between theory and operational practicevan Hengel, C. / Kortbeek, P. et al. | 2009
- 619
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Detailed strain field analyses of fatigue cracks in friction stir welded jointsLemmen, H.J.K. / Alderliesten, R.C. / Benedictus, R. et al. | 2009
- 643
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A study of interaction and coalescence of micro surface fatigue cracks in aluminium 7050Hu, W. / Liu, Q. / Barter, S. et al. | 2009
- 661
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Fracture behaviour of skin materials of civil airplane structuresNesterenko, B. / Nesterenko, G.I. / Basov, V.N. et al. | 2009
- 685
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Fatigue life prediction of small notched TI-6AL-4V based on the theory of critical distanceYamashita, Y. / Shinozaki, M. / Kuroki, H. / Ueda, Y. et al. | 2009
- 707
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A case study of multiple-site fatigue crack growth in the F-18 Hornet bulkheadAndersson, B. / Blom, A.F. / Falk, U. / Wang, G.S. / Koski, K. / Siljander, A. / Linna, J. / Miettinen, A. / Vaaraniemi, K. / Lahtinen, R. et al. | 2009
- 743
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Experimental and theoretical comparison of some multiaxial fatigue design criteria in the context of life assessment of rotating parts in turboenginesBonnand, V. / Chaboche, J.L. / Cherouali, H. / Gomez, P. / Kanoute, P. / Pacou, D. / Paulmier, P. / Ostoja-Kuczynski, E. / Vogel, F. et al. | 2009
- 765
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A contribution of environmental investigations for Glare riveted joint sizingBeumler, T. / Borgonje, B. / Sinke, J. et al. | 2009
- 789
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Advances in crack growth modelling of 3D aircraft structuresMellings, S.C. / Baynham, J.M.W. / Adey, R.A. et al. | 2009
- 811
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Development of advanced risk assessment methodologies for aircraft structures containing MSD/MEDLiao, M. / Bombardier, Y. / Renaud, G. / Bellinger, N. / Cheung, T. et al. | 2009
- 839
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Crack growth in fibre metal laminates under variable amplitude loadingKhan, S.U. / Alderliesten, R.C. / Benedictus, R. et al. | 2009
- 839
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Crack growth in fiber metal laminates under variable amplitude loadingKhan, S.U. / Alderliesten, R.C. / Benedictus, R. et al. | 2009
- 859
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Effect of residual stresses from shot peening on fatigue strength and threshold to crack propagation of AL 7475 alloy componentsRatti, G. / Mariani, U. / Giglio, M. / Guagliano, M. et al. | 2009
- 871
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Experimental validation of stress intensity factor solutions for the pin loaded lugChild, D.R. / Moyle, N.J. / Grandt, A.F. et al. | 2009
- 899
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Properties of fatigue crack propagation in friction stir welded 2024-T3 aluminum alloyOkada, T. / Kuwayama, K. / Fujita, S. / Asakawa, M. / Nakamura, T. / Machida, S. et al. | 2009
- 899
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Properties of fatigue crack propagation in friction stir welded 2O24-T3 aluminum alloyOkada, T. / Kuwayama, K. / Fujita, S. / Asakawa, M. / Nakamura, T. / Machida, S. et al. | 2009
- 909
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Fatigue crack growth in thick plate 7050 aluminumSchubbe, J. et al. | 2009
- 921
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Fatigue life evaluation on tension type fittingBarea, N. / Masse, M. et al. | 2009
- 931
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Accelerated fatigue testing on hydraulic shakerFressinet, M. / Panis, M. / Bordes, C. et al. | 2009
- 939
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Methods for FEM analysis of riveted joints of thin-walled aircraft structures within the Imperja projectKaniowski, J. / Wronicz, W. / Jachimowicz, J. / Szymczyk, E. et al. | 2009
- 969
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On the crack growth behaviour under simple compressive loads of 2024-T3 aluminium alloyKrkoska, M. / Alderliesten, R.C. / Benedictus, R. et al. | 2009
- 969
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On the crack growth behavior under simple compressive loads of 2O24-T3 aluminium alloyKrkoska, M. / Alderliesten, R.C. / Benedictus, R. et al. | 2009
- 987
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An analytical model for load transfer in a mechanically fastened, double-lap jointPaletti, L. / Rans, C. / Benedictus, R. et al. | 2009
- 1005
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Simulation of fatigue crack growth in the high speed machined panel under the constant amplitude and spectrum loadingAugustin, P. et al. | 2009
- 1019
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Bonded composite patch to repair metallic structures: Disbond propagation testing and modellingMadelpech, P. / Juaneda, S. / Pradels, M. et al. | 2009
- 1035
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Three dimensional crack growth predictionGalyon, S.E. / Arunachalam, S.R. / Greer, J. / Hammond, M. / Fawaz, S.A. et al. | 2009
- 1035
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Three diminsional crack growth predictionGalyon, Sarah E. / Arunachalam, Saravanan R. / Greer, James / Hammond, Matthew / Fawaz, Scott A. et al. | 2009
- 1069
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Hybrid structures for concentrated load transmission in fibre composites: Initial experimentsVermeer, P. / Alderliesten, R. / Benedictus, R. et al. | 2009
- 1085
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Pilatus PC-21 - A damage tolerant aircraftSchmid, L. et al. | 2009
- 1093
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Introduction to service of an artificial neural network based fatigue monitoring systemReed, S. / McCoubrey, B. / Mountfort, A. et al. | 2009
- 1121
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Towards automated flight-maneuver-specific fatigue analysisJylha, J. / Ruotsalainen, M. / Salonen, T. / Janhunen, H. / Viitanen, T. / Vihonen, J. / Visa, A. et al. | 2009
- 1135
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Service history analysis and teardown evidence - Key elements for structural usage monitoring of an ageing fleetLucas, K.A. / Duffield, M.J. et al. | 2009
- 1155
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Development of fatigue life monitoring of RMAF fighter airplanesKuntjoro, W. / Ashari, M.S. / Ahmad, M.Y. / Mydin, A.M. et al. | 2009
- 1165
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Research and development of impact damage detection system for airframe structures using optical fiber sensorsTsutsui, H. / Hirano, N. / Kimoto, J. / Akatsuka, T. / Sashikuma, H. / Takeda, N. / Tajima, N. et al. | 2009
- 1177
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Load factors (N/Z) / roll rate: First comparisons between design and inflight recorded data on Eurofighter typhoon Italian fleetGiacobbe, T. / Sardo, F. et al. | 2009
- 1187
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Development of a structural health monitoring system to evaluate debonding in composite adhesive structuresSoejima, H. / Nakamura, N. / Ogisu, T. / Wakai, H. / Okabe, Y. / Takeda, N. / Koshioka, Y. et al. | 2009
- 1199
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OLM: A hands-on approachWillis, S. et al. | 2009
- 1215
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F-35 Joint strike fighter structural prognosis and health management: An overviewFallon, T. / Mahal, D. / Hebden, I. et al. | 2009
- 1219
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Bonded repair for fuselage damage: An overall benefit to commercial aviationFurfari, D. / Woerden, H.J.M. / Benedictus, R. / Kwakernaak, A. et al. | 2009
- 1245
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Fatigue & damage tolerance of hybrid materials & structures - Some myths, facts & fairytalesAlderliesten, R.C. et al. | 2009
- 1261
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High cycle fatigue of laser beam deposited Ti-6Al-4V and inconel 718Amsterdam, E. / Kool, G.A. et al. | 2009
- 1275
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The variable expansion process - A new cost efficient method for cold working fasterner holes in aluminium aircraft structuresReese, E.D. / Dowson, A.L. / Jones, T.G.B. et al. | 2009
- 1275
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The variable expansion process - a new cost efficient method for cold working fastener holes in aluminium aircraft structuresReese, Eggert D. / Dowson, Anthony L. / Jones, Timothy G.B. et al. | 2009
- 1285
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Stress measurements with x-ray diffractometry on aluminium alloys. Determination of the most optimized parameters of the measurementGadalinska, E. / Kaniowski, J. / Wojtas, A. et al. | 2009
- 1305
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Delamination growth at interfaces in hybrid materials and structures under various opening modesDelgrange, G. / Alderliesten, R.C. / Benedictus, R. et al. | 2009
- 1321
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Developments in metal bondingAakkula, J.J. / Lumppio, K. / Saarela, O. / Haikola, T. et al. | 2009
- 1345
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On separating the effect of corrosion on inter-lamellar fatigue on thin sheet AA7079-T6Shah, S.R. / Fawaz, S.A. et al. | 2009