data. Pp. 541–556 in Small Fatigue Cracks. Warrendale, Pennsylvania: The Minerals, Metals, and Materials Society.

Bucci, R., R. Bush, A. Hinkle, H. Konish, M. Kulak, and R. Wygonik. 1996. High-strength aluminum forged product durability and damage tolerance for weight and total life cost saving. Pp. 681–702 in Proceedings of the 1995 USAF Aircraft Structural Integrity Program Conference, Vol. 2. WL-TR-96-4094. Wright-Patterson AFB, Ohio: Wright Aeronautical Laboratories.

Buchheit, R.G. in press. Copper removal during formation of corrosion resistant alkaline oxide coatings on Al-Cu-Mg alloys. Journal of Applied Electrochemistry.

Cannava, V. 1997. LogisTech, Inc. Personal communication, April 10, 1997.

Chu, R.C., and T.C. Ko. 1989. Isoparametric shear spring element applied to crack patching and instability. Theoretical and Applied Fracture Mechanics 11:93–102.

Coffey, J.M., and R.K. Chapman. 1983. Applications of elastic scattering theory for smooth flat cracks to the quantitative prediction of ultrasonic defect detection and sizing. Nuclear Energy 22(5):319–333.

Cowie, W.D. 1989. Fracture control philosophy. Pp. 666–673 in Metals Handbook, Volume 17: Nondestructive Evaluation and Quality Control. Metals Park, Ohio: ASM International.


Dexter, H.B., and D.J. Baker. 1994. Flight service environmental effects on composite materials and structures. Advanced Performance Materials 1(1):51–85.

DOD (U.S. Department of Defense). 1987. Airplane Damage Tolerance Requirements. MIL-A-83444. Washington, D.C.: U.S. Department of Defense.

DOD. 1988. Aircraft Structural Integrity Program Airplane Requirements. MIL-STD-1530, revision A. Washington, D.C.: U.S. Department of Defense.

DOD. 1994. Polymer Matrix Composites, Vol. 1. MIL-HNBK-17. Washington, D.C.: U.S. Department of Defense.

Donley, M.S. 1996. Advanced Aircraft Coatings: Program Overview. Presentation to the Committee on Aging of U.S. Air Force Aircraft, National Materials Advisory Board, National Research Council, Wright-Patterson AFB, Ohio, August 22.

Dubois, J.M., S.K. Song, and Y. Massiani. 1993. Application of quasicrystalline alloys to surface coating of soft metals. Journal of Non-Crystalline Solids 153–154:443–445.


Elshafiey, I., and J. Gray. 1996. Optimization tool for x-ray radiography. Pp. 425–432 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 15. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press.

Emeric, P.R., and W.P. Winfree. 1995. Thermal characterization of multilayer structures from transient thermal response. Pp. 475–482 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 14. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press.

Erdogan, F., and K. Arin. 1972. A sandwich plate with a part-through and a debonding crack. Engineering Fracture Mechanics 4:449–458.


FAA (Federal Aviation Administration). 1996. Airworthiness Assurance R&D Branch: Research Accomplishments, 1996. Atlantic City, N.J.: FAA Technical Center.

Favro, L.D., X. Han, Y. Wang, P.K. Kuo, and R.L. Thomas. 1995. Pulsed echo thermal wave imaging. Pp 425–429 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 14. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press.

Favro, L.D., X. Han, T. Ahmed, P.K. Kuo, and R.L. Thomas. 1996. Measuring corrosion thinning by thermal wave imaging. Pp. 374–379 in SPIE Proceedings, Vol. 2945. NDE of Aging Aircraft, Airports, and Aerospace Hardware. R.D. Rempt and A. Broz, eds. Bellingham, Washington: Society of Photo-Optical Instrumentation Engineers.

Fitzpatrick, G.L., D.D. Thome, R.L. Skaugset, and W.C.K. Shih. 1996. Magneto-optic eddy current imaging of sub-surface corrosion and fatigue cracks in aging aircraft . Pp. 1159–1165 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 15. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press.

Fredell, R.S. 1994. Damage tolerant repair techniques for pressurized aircraft fuselages. Ph.D. dissertation, Aerospace Engineering, Delft University of Technology, The Netherlands.

Fredell, R., C. Guijt, D. Conley, and S. Knighton. 1996. Design development of a bonded fuselage repair for the C-5A. Pp. 887–902 in Proceedings of the 1995 USAF Aircraft Structural Integrity Program Conference, Vol. 2. WL-TR-96-4094. Wright-Patterson AFB, Ohio: Wright Aeronautical Laboratories.


Geng, Z.J., G.G. Pan, W.S. Haynes, B.K. Wada, and J.A. Gorba. 1994. Six degree of freedom active vibration isolation and suppression experiments. Pp. 285–294 in Proceedings of the Fifth International Conference on Adaptive Structures. J. Tani, ed. Basel, Switzerland: Technomic.

Goering, J., and J. Dominguez. 1992. Large Scale Structural Damage Repair Analysis. Presentation at the 24th International SAMPE (Society for the Advancement of Materials and Process Engineering) Technical Conference, Toronto, Canada, October 20–22.

Goranson, U.G. 1997. Structural Airworthiness Initiatives. Presentation at the DoD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, July 8–10.

Gray, T.A., and R.B. Thompson. 1986. Use of models to predict ultrasonic NDE reliability. Pp. 911–918 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 5. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press.


Hagemaier, D., and A. Hoggard. 1993. NDI technology as it relates to aging aircraft. Materials Evaluation 51(12):1360–1368.



The National Academies | 500 Fifth St. N.W. | Washington, D.C. 20001
Copyright © National Academy of Sciences. All rights reserved.
Terms of Use and Privacy Statement