Structural Integrity of Aging Airplanes
The emergence of civil aviation as a means of mass transportation is primarily due to the large scale construction of jet airplanes in the past 30 years or so. A large number of these jet airplanes is currently operating at or beyond their designed fatigue lives. Thus, the structural integrity of t...
| Other Authors: | , , |
|---|---|
| Format: | eBook |
| Language: | English |
| Published: |
Berlin, Heidelberg
Springer Berlin Heidelberg
1991, 1991
|
| Edition: | 1st ed. 1991 |
| Series: | Springer Series in Computational Mechanics
|
| Subjects: | |
| Online Access: | |
| Collection: | Springer Book Archives -2004 - Collection details see MPG.ReNa |
Table of Contents:
- 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
- 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