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8
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Fatigue crack growth characterization of jet transport structures
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Ottawa, Canada, June 8-12
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Miller, M., Luthra, V. K. and Goranson, U. G., Fatigue crack growth characterization of jet transport structures. 14th Symposium of the International Committee on Aeronautical Fatigue (ICAF), Ottawa, Canada, June 8-12, 1987.
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Miller, M.1
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Damage tolerance in pressurized fuselages
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Aging jet transport structural evaluation programs
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Jerusalem, Israel, June 21-23
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Goranson, U. G. and Miller, M., Aging jet transport structural evaluation programs. 15th Symposium of the International Committee on Aeronautical Fatigue (ICAF), Jerusalem, Israel, June 21-23, 1989.
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Goranson, U.G.1
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Durability and damage tolerance evaluations of jet transport structures
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Whittaker, I. C., Miller, M. and Goranson, U. G., Durability and damage tolerance evaluations of jet transport structures. 5th International Conference on Structural Safety and Reliability (ICOSSAR), San Francisco, CA, August 1989.
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The prospect of detecting and dealing with widespread fatigue damage: Threshold for inspecting MSD susceptible lap spices
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Melbourne, Australia, August 26-28
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Sampath, S. G. and Broek, D., The prospect of detecting and dealing with widespread fatigue damage: threshold for inspecting MSD susceptible lap spices. International Conference on Aircraft Damage Assessment and Repair, Melbourne, Australia, August 26-28, 1991.
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Fleet fatigue cracking threshold prediction
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Tokyo, Japan, May 20-24
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Whittaker, I. C., Stilwell, P. B. and Sizemore, D. R., Fleet fatigue cracking threshold prediction. 16th Symposium of the International Committee on Aeronautical Fatigue (ICAF), Tokyo, Japan, May 20-24, 1991.
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Results of the AAWG industry committee on widespread fatigue damage
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Atlanta, GA, March 31-April 2
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Thomson, D., Hoadley, D. and McHatton, J., Load tests of flat and curved panels with multiple cracks. Foster-Miller Draft Final Report to the FAA Center, September 1993.
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Load Tests of Flat and Curved Panels with Multiple Cracks
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Atlantic City, NJ, June 27-28
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Bigelow, C. A. and Tan, P. W., An integrated methodology for assessing widespread fatigue damage in aircraft structures. Proceedings of the FAA-NASA 6th International Conference on the Continued Airworthiness of Aircraft Structures, Atlantic City, NJ, June 27-28, 1995, pp. 121-138.
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Fracture testing of large-scale thin-sheet aluminum alloy
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Harris, C. E., Starnes Jr., J. H. and Newman Jr., J. C., Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures. Proceedings of the FAA-NASA 6th International Conference on the Continued Airworthiness of Aircraft Structures, Atlantic City, NJ, June 27-28, 1995, pp. 139-164.
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Newman Jr., J. C. and Dawicke, D. S., Fracture analysis of stiffened panels under biaxial loading with widespread cracking. NASA Report TM 110197, November 1995.
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Wang, L., Brust, F. W. and Atluri, S. N., Computational predictions of the NIST multiple site damage experimental results. FAA Center of Excellence Report, Georgia Institute of Technology, August 1995.
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