Author:
Kale Amit,Haftka Raphael,Papila Melih,Sankar Bhavani
Publisher
American Institute of Aeronautics and Astronautics
Reference14 articles.
1. Arietta, A. J., Striz, A. G."Modelling of Aircraft FatigueLoadEnvironment,"38th Aerospace Sciences Meeting and Exhibit, Paper AIAA-00-0973, 10-13January 2000, Reno, Nevada
2. Arietta, A. J., Striz, A. G. and Venkayya, V. B. "An Approach to The Design of Aircraft Structures with Damage Tolerance Requirements,"41stAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Paper AIAA-00-1786, 3-6April 2000, Atlanta, GA. Symposium on Multidisciplinary AnalysisandOptimization, Paper AIAA-00-4925, 6-8 September 2000,LongBeach,CA.
3. Backman, B., 2001, "Structural Design Performed to Explicit Safety Criteria Containing Uncertainties," 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, AIAA-01-25046, 16-19April2001,Seattle,Washington.
4. Brot, A., 1994, "Probabilistic Inspection Strategies for Minimizing Service Failures," FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, September1994.PartI,p.99-109
5. An optimal inspection strategy for randomly failing equipment
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Reliability Based Design and Inspection of Stiffened Panels Against Fatigue;46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2005-04-18