Tradeoff of structural weight and inspection cost in reliability based optimization using multiple inspection types

Collection of Technical Papers - 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference

Volumn 2, Issue , 2004, Pages 1162-1173

  Kale, Amit A ^a   Haftka, Raphael T ^a   Sankar, Bhavani V ^a  

^a J Crayton Pruitt Family Department of Biomedical Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

INSPECTION COSTS; MULTIPLE INSPECTION; RELIABILITY BASED OPTIMIZATION; STRUCTURAL WEIGHT;

AIRCRAFT; FATIGUE OF MATERIALS; PROBLEM SOLVING; RELIABILITY; STRESS INTENSITY FACTORS; STRUCTURAL ANALYSIS;

STRUCTURAL OPTIMIZATION;

EID: 20344380695     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (29)

1. Arietta, A. J., Striz, A. G., "Modelling of Aircraft Fatigue Load Environment," 38th Aerospace Sciences Meeting and Exhibit, Paper AIAA-00-0973, 10-13 January 2000, Reno, Nevada.
2. st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Paper AIAA-00-1786, 3-6 April 2000, Atlanta, GA.
3. Symposium on Multidisciplinary Analysis and Optimization, Paper AIAA-00-4925, 6-8 September 2000, Long Beach, CA..
4. 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, 16-19 April 2001, Seattle, Washington.
5. Backman, B., 2001,"Reliability based Structural Design with Uncertainties and Special Knowledge of Growth"[unpublished]).
6. Bergner, F., Zouhar G.,"A new approach to the correlation between the coefficient and exponent in the power law equation of fatigue crack growth". International journal of Fatigue 22 (2000) 229-329.
7. 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, September 1994. Part I, p.99-109.
8. Chang, J. B., Szamossi, M. and Liu, K.W., "Random Spectrum fatigue Crack Life Predictions With or Without Considering Load Interaction. Methods and models for predicting fatigue crack growth under random loading. ASTM special technical publication, 748, 1981.
9. Chelbi, A., Ait-Kadi, D., "An optimal inspection strategy for randomly failing equipment". Reliability Engineering and systems safety 63 (1999) 127-131.
10. Dolenski, K., Colombi, P.," Fatigue lifetime under stochastic loading with random overloading pulse train." Computer Methods in applied mechanics and engineering 168 (1999) 221-241.
11. th International symposium on Nondestructive evaluation and health monitoring of aging infrastructure, Newport beach, CA, March 2000.
12. Fujimoto, Y., Kim, S.C., Hamada, K., Huang, F., "Inspection Planning Using Genetic Algorithm for Fatigue Deteriorating Structures", Proceedings of the International Offshore and Polar Engineering Conference v 4 1998. ISOPE, Golden, CO, USA. P 461-468.
13. Garbatov, Y., Soares, C.G., "Cost and reliability based strategies for fatigue Toyoda-Makino maintenance planning of floating structures. Reliability Engineering and Systems Safety 73 (2001) 293-301.
14. Harkness, H. A., Fleming, M., Moran, B., Belytschko, T., 1994, "Fatigue Reliability Method with In-Service Inspections," FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, September 1994. Part I, p 307-325.
15. Hudson, C. M.,"A root -mean-square approach for predicting fatigue crack growth under random loading". Methods and models for predicting fatigue crack growth under random loading. ASTM special technical publication 748, 1981.
16. Johnson, W.S., "Multi parameter yield zone model for predicting spectrum crack growth". Methods and models for predicting fatigue crack growth under random loading. ASTM special technical publication, 748, 1981
17. st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Paper AIAA-00-1371, 3-6 April 2000, Atlanta, GA.
18. Massarelli, P.J. and Baber, T.T.,"Fatigue Reliability of Steel Highway Bridge Details". [Unpublished] Final report, Virginia Transport research Council, Charlottesville Virginia.
19. Nees, C. D. and Canfield, R. A., 1998, "Methodology for Implementing Fracture Mechanics in Global Structural Design of Aircraft," Journal of Aircraft, 35 (1), pp. 131-138.
20. Newman, J.C Jr., "A crack closure model for predicting fatigue crack growth under aircraft spectrum loading". Methods and models for predicting fatigue crack growth under random loading. ASTM special technical publication 748, 1981.
21. Niu, M., C., Airframe Structural Design, 1990, Chapter 15.0 Fatigue, Damage Tolerance and Fail-Safe Design, p 538-570.
22. Provan, J.W., and Farhangdoost, K., 1994,"A new Stochastic Systems Approach to Structural Integrity" FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance September 1994. Part I, p 603-619.
23. Rudd, J.L. and Engle R.M., "Crack Growth Behavior of Centre-Cracked Panels under random Spectrum Loading". Methods and models for predicting fatigue crack growth under random loading. ASTM special technical publication, 748, 1981.
24. J.F. Schutte, J.A. Reinbolt, B.J. Fregly and R.T. Haftka. Parallel Global Optimization with the Particle Swarm Algorithm. J. Numer. Meth. Eng. (In Print).
25. Tisseyre, M., Plantec, J.Y., Beaufils, J.Y., Boetsch, R. "Aerospatiale Probabilistic Methods Applied to aircraft maintenance, 1981.
26. Toyoda-Makino, M., "Cost-based optimal history dependent strategy for random fatigue cracks growth". Probabilistic Engineering Mechanics 14 (1999) 339-347
27. Venter, G. "Non-dimensional Response Surfaces for Structural Optimization with Uncertainty,"Ph.D. dissertation, University of Florida, 1998.
28. st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Paper AIAA-00-1371, 3-6 April 2000, Atlanta, GA.
29. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Paper AIAA-04-1789, 19-22 April 2003, Palm Springs, CA.