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
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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| Hovedforfatter: | |
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| Format: | Livre numérique |
| Sprog: | Anglais |
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Dordrecht :
Springer Netherlands
[20..].
Cham : Springer Nature |
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| Online adgang: | Accès sur la plateforme de l'éditeur Accès sur la plateforme Istex Accès Université d'Orléans Accès INSA CVL |
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Archives Springer e-books (Licence nationale) Archives Springer e-books (Licence nationale) |
| Autres localisations: | Voir dans le Sudoc |
| Edition sous un autre format: | • ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives, 9789400716636 • ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives, 9789400716650 • ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives, 9789401778824 |
Indholdsfortegnelse:
- TABLE OF CONTENTS PLANTEMA MEMORIAL LECTURE: Fleet recovery and life extension - Some lessons learned, by G. Clark AIRWORTHINESS AND OTHER CONSIDERATIONS: Sticks and stones (Could the words of aeronautical fatigue hurt us?), by S. Swift Analysis of requirements on fatigue and damage tolerance for civil transport airplanes, by B.G. Nesterenko, G.I. Nesterenko Material selection and detailed design - Requirements and responsibilities of an accredited and qualified test laboratory, by J. Gruner, S. Reichard, S. Goldbach, J. Ridzewski, R. Franke, R. Best, Th. Fleischer ADVANCED MATERIALS AND INNOVATIVE STRUCTURAL CONCEPTS: Bombardier aerospace FSW demonstrator, by L.J.J. Kok, K. Poston, G. Moore Evaluation of fatigue crack growth behavior in FSW joint by experiment, analysis and elasto-plastic FEM, by T. Okada, K. Kuwayama, M. Asakawa, T. Nakamura, S. Machida, S. Fujita, H. Terada Recent development on bonded structures, by G. Delgrange, J.C. Ehrström Recent advancements in thin-walled hybrid structural technologies for damage tolerant aircraft fuselage applications, by R.C. Alderliesten, C.D. Rans, Th. Beumler, R. Benedictus Fatigue life assessment for composite structure, by A. Makeev, Y. Nikishkov Potential of CFRP used for light weight structures: Some experimental results, by Th. Fleischer, J. Ridzewski, M. Sachse, F. Schirmacher An implementation of an accelerated testing methodology to obtain static, creep and fatigue master curves of a T300/913 unidirectional composite material, by Y. Freed, S. Rzepka Improvement of vibration damping and flexural fatigue property incorporating nanoclay into glass/epoxy composite, by A. Kabir, S.V. Hoa Formation of a metal coating by means of friction stir processing, by D. Kocańda, A. Górka, D. Zasada Influence of the carbon nanotube type, loading and chemical functionalization on the fatigue resistance of aluminum lap joints, by I.D. Rosca, R. Mactabi, S.V. Hoa Fatigue damage behavior of glass/epoxy composites using carbon nanotubes as sensors, by H. Hena-Zamal, S.V. Hoa DSTO - NLR Collaborative programme on fatigue properties of beta-annealed Ti-6Al-4V: Preliminary results, by E. Amsterdam, A. Shekhter, S.A. Barter, M. McDonald, R.J.H. Wanhill Damage tolerance demonstration of flange joint for aircraft engine composite fan case, by Y. Ueda, H. Kuroki, T. Murooka, A. Tanaka, K. Miyazawa, I. Okumura, Y. Shigenari, K. Oikawa, H. Morita FATIGUE CRACK GROWTH AND LIFE PREDICTION METHODS: The formation/nucleation of fatigue cracks in aircraft structural materials, by D.W. Hoeppner Modelling of continuing damage for damage tolerance analysis, by Y. Bombardier, M. Liao, G. Renaud The critical importance of correctly characterising fatigue crack growth rates in the threshold regime, by K.F. Walker, S.A. Barter The relationships between crack closure, specimen compliance and effective fatigue crack growth rate, by D.L. Ball, J.K. Donald, M.A. James, R.J. Bucci Experimental and numerical study of stress and strain field around the rivet, by W. Wronicz, J. Kaniowski, B. Korzeniewski, E. Gadalinska Fatigue analyses of riveted lap-splice joints in a narrow-body aircraft, by J.C. Newman Jr., R. Ramakrishnan Crack growth rate curves: Which part dominates life prediction and when?, by C. Wallbrink, P. Jackson, W. Hu Critical distance for fatigue life prediction in aerospace materials, by Y. Yamashita, Y. Ueda, H. Kuroki A unified variable amplitude model for crack initiation and crack propagation, by A.B. Chattopadhyay, G. Glinka Development of an efficient methodology and tool to determine stress intensity correction factors for complex aircraft structures, by G. Renaud, M. Liao, Y. Bombardier Improved SIF calculation in riveted panel type structures using numerical simulation, by S.C. Mellings, J.M.W. Baynham, T.J. Curtin An 1D-Beam approach for both stress analysis and fatigue life prediction of bonded joints, by E. Paroissien, A. Da Veiga, A. Laborde Cyclic stress-strain and strain-life properties of aerospace metallic materials, by S.K. Walker, A.C. Quilter Crack propagation calculation for aluminium aircraft structures considering the influence of load sequences, by R. Buchholz Analysis of fatigue crack growth under random load sequences derived from military in-flight load data, by C. Mattrand, J.-M. Bourinet, D. Théret, M. Lemaire, P. Bernard, M. Fogli Statistical analysis of fatigue crack growth based on the unigrow model, by S. Mikheevskiy, S. Bogdanov, G. Glinka Fatigue life estimation of structures subjected to vibratory loading, by M. Fressinet, F. Fuchs, P. Madelpech A structural defect expansion model based on physical correlation, by S. Ito, S. Sugimoto, T. Okada STRUCTURAL HEALTH AND STRUCTURAL LOADS MONITORING: Link between flight maneuvers and fatigue J. Jylhä, M. Ruotsalainen, T. Salonen, H. Janhunen, I. Venäläinen, A. Siljander, A. Visa Health and usage monitoring of unmanned aerial vehicles using fiber-optic sensors I. Kressel, A. Handelman, Y. Botsev, J. Balter, P. Gud's, M. Tur, S. Gali, A.C.R. Pillai, M.H. Prasad, A.K. Yadav, N. Gupta, S. Sathya, R. Sundaram Airframe loads & usage monitoring of the CH-47D "Chinook" helicopter of the Royal Netherlands Air Force, by A. Oldersma, M.J. Bos Damage detection system for automated hot spot monitoring based on different technologies used in component testing for shot peening validation, by C. Stolz, M. Neumair, L. Benassi Memorization and detection of an arrested crack in foam-core sandwich structures using embedded metal wires and fiber-optic sensors, by S. Minakuchi, N. Takeda, Y. Hirose Structural load monitoring systems for military aircraft in the Polish armed forces with examples of selected activities, by M. Kurdelski, S. Klimaszewski, A. Leski FULL SCALE FATIGUE TESTING OF AIRCRAFT AND AIRCRAFT COMPONENTS: A320 ESG Full scale fatigue test-Lessons learned, by G. Hilfer, N. Roessler, C. Peters, C. Herrmann New connection strap concepts for A320 wheel well area tested during the airbus A320 extended service goal full scale fatigue test, by N. Cenic, B. Zapf, T. Haberle Full-scale static and fatigue testing of composite fuselage section, by R. Kothari Durability and damage tolerance evaluation of VaRTM composite wing structure, by Y. Aoki, Y Hirano, S. Sugimoto, Y. Iwahori, Y. Nagao, T. Ohnuki Development of load spectrum for full scale fatigue test of a trainer aircraft, by A. Leski, P. Reymer, M. Kurdelski INSERVICE EXPERIENCE, LIFE EXTENSION AND MANAGEMENT OF AGEING FLEETS: ATR Life extension project, by M. Cajani, R. Ciotola, J. David, J. Salvi Benefits of using a risk process in ASIP - The CF-18 experience, by Y. Beauvais Integrated probabilistic analysis of damage tolerance and risk for airframe structural locations, by W. Hu, R.F. Torregosa Aircraft joints and corrosion control, by U.H. Tiong, G. Clark A case study of nose landing gear failure caused by fatigue, by V.Y. Guertsman Test method for determining the effect of chromate primers on fatigue crack growth, by Y. Lee, S.E. Galyon Dorman, M.J. Hammond