Structural Integrity of Aging Airplanes: Springer Series in Computational Mechanics
Editat de Satya N. Atluri, Sam G. Sampath, Pin Tongen Limba Engleză Paperback – 21 dec 2011
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Specificații
ISBN-13: 9783642843662
ISBN-10: 3642843662
Pagini: 512
Ilustrații: XII, 496 p.
Dimensiuni: 155 x 235 x 27 mm
Greutate: 0.71 kg
Ediția:Softcover reprint of the original 1st ed. 1991
Editura: Springer Berlin, Heidelberg
Colecția Springer
Seria Springer Series in Computational Mechanics
Locul publicării:Berlin, Heidelberg, Germany
ISBN-10: 3642843662
Pagini: 512
Ilustrații: XII, 496 p.
Dimensiuni: 155 x 235 x 27 mm
Greutate: 0.71 kg
Ediția:Softcover reprint of the original 1st ed. 1991
Editura: Springer Berlin, Heidelberg
Colecția Springer
Seria Springer Series in Computational Mechanics
Locul publicării:Berlin, Heidelberg, Germany
Public țintă
ResearchCuprins
1. Towards Quantitative Non-Destructive Evaluation of Aging Aircraft.- 2. Computational Schemes for Integrity Analyses of Fuselage Panels in Aging Airplanes.- 3. Risk Analysis for Aging Aircraft Fleets.- 4. Aspects of Aging Aircraft: A TransAtlantic View.- 5. The Civil Damage Tolerance Requirements in Theory and Practice.- 6. The Effect of Exfoliation Corrosion on the Fatigue Behavior of Structural Aluminum Alloys.- 7. A Damage Tolerance Approach for Management of Aging Gas Turbine Engines.- 8. An Evaluation of the Pressure Proof Test Concept for 2024-T3 Aluminum Alloy Sheet.- 9. Aging Jet Transport Structural Evaluation Programs.- 10. NASA Airframe Structural Integrity Program.- 11. The Aloha Airlines Accident — A New Era for Aging Aircraft.- 12. Fuselage Longitudinal Splice Design.- 13. Representation and Probability Issues in the Simulation of Multi-Site Damage.- 14. Bonded Repair of Multi-Site Damage.- 15. Applications of Advanced Fracture Mechanics to Fuselage.- 16. Axial Crack Propagation and Arrest in Pressurized Fuselage.- 17. Structural Integrity of Aging Airplanes: A Perspective.- 18. A Laboratory Study of Fracture in the Presence of Lap Splice Multiple Site Damage.- 19. How Likely is Multiple Site Damage?.- 20. Fractographic Analysis of Initiation and Growth of Fatigue Cracks at Rivet Holes.- 21. Results of Review of Fokker F28 “Fellowship” Maintenance Program.- 22. Test Facility for Evaluation of Structural Integrity of Stiffened & Jointed Aircraft Curved Panels.- 23. Estimation of Requirements of Inspection Intervals for Panels Susceptible to Multiple Site Damage.- 24. Evaluation Methodologies Applied for Pressurized Fuselages of Airbus A/C.- 25. Experience in Specifying/Prolonging the Airframe Time Limits.- 26. Optical Methods of Stress AnalysisApplied to Cracked Components.- 27. Repairs to Damage Tolerant Aircraft.- 28. Case Study and Simulation of Fatigue Damages and DTE of Aging Aircraft — A Review of Researches in Japan.