References

AGARD (Advisory Group for Aerospace Research and Development). 1990. Short-Crack Growth Behaviour in Various Aircraft Materials. P. R. Edwards and J. C. Newman, Jr., compilers, AGARD-R-767. Neuilly-Sur Seine, France: North Atlantic Treaty Organization.

AGARD. 1992. Environmentally Safe and Effective Processes for Paint Removal, AGARD-CP-791. Neuilly-Sur Seine, France: North Atlantic Treaty Organization.

AGARD. 1996. Environmentally Compliant Surface Treatments of Materials for Aerospace Applications, AGARD-CP-816. Neuilly-Sur Seine, France: North Atlantic Treaty Organization.

Agarwala, V.S., and A. Fabiszewski. 1994. Think Film Microsensors for Integrity of Coatings, Composites, and Hidden Structures. Presentation at the 1994 NACE International Corrosion Conference, Baltimore, Maryland, March.

Agarwala, V.S., P.K. Bhagat, and G.L. Hardy. 1995. Corrosion detection and monitoring of aircraft structures: An overview. Pp. 19-1–19-6 in Corrosion Detection and Management of Advanced Airframe Materials, AGARD-CP-565. Advisory Group for Aerospace Research and Development. Neuilly-Sur Seine, France: North Atlantic Treaty Organization.

ASM. 1987. Metals Handbook, Vol. 13. Corrosion. Metals Park, Ohio: ASM International.

Atluri, S.N. 1997. Structural Integrity and Durability. Forsyth, Georgia: Tech Science Press.

Atluri, S.N., and K. Kathiresan. 1978. Stress analysis of typical flaws in aerospace structural components using 3D hybrid displacement finite element method. Pp. 340–351 in Proceedings of the 19th AIAA/ASME Structures, Structural Dynamics, and Materials Conference. New York: American Institute of Aeronautics and Astronautics.


Bakuckas, J.G., C.C. Chen, P.W. Tan, and C.A. Bigelow. 1996. Engineering Approach To Damage Tolerance Analysis of Fuselage Skin Repairs. DOT/FAA/CT-95/75. Atlantic City, N.J.: Federal Aviation Administration Technical Center.

Barnard, D.J., and D.K. Hsu. 1997. Development and testing of the dripless bubbler ultrasonic scanner. Pp. 2069–2076 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 16. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press.

Beier, T.H. 1997a. Sonic fatigue—A problem requiring special handling. Pp. 597–612 in Proceedings of the 1996 USAF Aircraft Structural Integrity Conference. WL-TR-97-4055. Wright-Patterson AFB, Ohio: Wright Aeronautical Laboratories.

Beier, T.H. 1997b. Effective Buffet Load Alleviation Via an Active Control Surface. Presentation at the DoD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, July 8–10.

Bellon, C., G. Tillack, C. Nockermann, and L. Stenzel. 1997. Computer simulation of x-ray NDE process coupled with CAD interface. Pp. 325–330 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 16. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press.

Berens, A.P. 1989. NDE reliability data analysis. Pp. 689–701 in Metals Handbook, Volume 17: Nondestructive Evaluation and Quality Control. Metals Park, Ohio: ASM International.

Bieber, J.A., S.K. Shaligran, J.N. Rose, and J.C. Moulder. 1997. Time-gating of pulsed eddy current signals for defect characterization and discrimination in aircraft lap-joints. Pp. 1915–1922 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 16. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press.

Blohowiak, K.Y., J.H. Osborne, K.A. Krienke, and D.F. Sekits. 1997. Durable Sol Gel Surface Preparations for Repair and Remanufacture of Aircraft Structures. Presentation at the DOD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, July 8–10.

Bodine, J.B., B.W. Flynn, M.H. Gessel, L.B. Ilcewicz, G.D. Swanson, M.F. Nahan, and J.R. Epperson. 1994. Repair of Composite Fuselage Panels. Paper presented at the Fifth NASA/DOD Advanced Composite Technology Conference, Seattle, Washington, August 22–25.

Boeing. 1994. Aging Airplane Corrosion Prevention and Control Program: Model 737-100/200. Document D6-38528, revision D. Seattle, Washington: Boeing Commercial Airplane Group.

Bucci, R.B., and C.J. Warren. 1997. Material Sunstitutions for Aging Aircraft. Presentation at the DoD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, July 8–10.

Bucci, R.B., R.L. Brazill, and J.R. Brockenbrough. 1986. Assessing growth of small flaws from residual strength



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Aging of U.S. Air Force Aircraft: Final Report References AGARD (Advisory Group for Aerospace Research and Development). 1990. Short-Crack Growth Behaviour in Various Aircraft Materials. P. R. Edwards and J. C. Newman, Jr., compilers, AGARD-R-767. Neuilly-Sur Seine, France: North Atlantic Treaty Organization. AGARD. 1992. Environmentally Safe and Effective Processes for Paint Removal, AGARD-CP-791. Neuilly-Sur Seine, France: North Atlantic Treaty Organization. AGARD. 1996. Environmentally Compliant Surface Treatments of Materials for Aerospace Applications, AGARD-CP-816. Neuilly-Sur Seine, France: North Atlantic Treaty Organization. Agarwala, V.S., and A. Fabiszewski. 1994. Think Film Microsensors for Integrity of Coatings, Composites, and Hidden Structures. Presentation at the 1994 NACE International Corrosion Conference, Baltimore, Maryland, March. Agarwala, V.S., P.K. Bhagat, and G.L. Hardy. 1995. Corrosion detection and monitoring of aircraft structures: An overview. Pp. 19-1–19-6 in Corrosion Detection and Management of Advanced Airframe Materials, AGARD-CP-565. Advisory Group for Aerospace Research and Development. Neuilly-Sur Seine, France: North Atlantic Treaty Organization. ASM. 1987. Metals Handbook, Vol. 13. Corrosion. Metals Park, Ohio: ASM International. Atluri, S.N. 1997. Structural Integrity and Durability. Forsyth, Georgia: Tech Science Press. Atluri, S.N., and K. Kathiresan. 1978. Stress analysis of typical flaws in aerospace structural components using 3D hybrid displacement finite element method. Pp. 340–351 in Proceedings of the 19th AIAA/ASME Structures, Structural Dynamics, and Materials Conference. New York: American Institute of Aeronautics and Astronautics. Bakuckas, J.G., C.C. Chen, P.W. Tan, and C.A. Bigelow. 1996. Engineering Approach To Damage Tolerance Analysis of Fuselage Skin Repairs. DOT/FAA/CT-95/75. Atlantic City, N.J.: Federal Aviation Administration Technical Center. Barnard, D.J., and D.K. Hsu. 1997. Development and testing of the dripless bubbler ultrasonic scanner. Pp. 2069–2076 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 16. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Beier, T.H. 1997a. Sonic fatigue—A problem requiring special handling. Pp. 597–612 in Proceedings of the 1996 USAF Aircraft Structural Integrity Conference. WL-TR-97-4055. Wright-Patterson AFB, Ohio: Wright Aeronautical Laboratories. Beier, T.H. 1997b. Effective Buffet Load Alleviation Via an Active Control Surface. Presentation at the DoD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, July 8–10. Bellon, C., G. Tillack, C. Nockermann, and L. Stenzel. 1997. Computer simulation of x-ray NDE process coupled with CAD interface. Pp. 325–330 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 16. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Berens, A.P. 1989. NDE reliability data analysis. Pp. 689–701 in Metals Handbook, Volume 17: Nondestructive Evaluation and Quality Control. Metals Park, Ohio: ASM International. Bieber, J.A., S.K. Shaligran, J.N. Rose, and J.C. Moulder. 1997. Time-gating of pulsed eddy current signals for defect characterization and discrimination in aircraft lap-joints. Pp. 1915–1922 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 16. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Blohowiak, K.Y., J.H. Osborne, K.A. Krienke, and D.F. Sekits. 1997. Durable Sol Gel Surface Preparations for Repair and Remanufacture of Aircraft Structures. Presentation at the DOD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, July 8–10. Bodine, J.B., B.W. Flynn, M.H. Gessel, L.B. Ilcewicz, G.D. Swanson, M.F. Nahan, and J.R. Epperson. 1994. Repair of Composite Fuselage Panels. Paper presented at the Fifth NASA/DOD Advanced Composite Technology Conference, Seattle, Washington, August 22–25. Boeing. 1994. Aging Airplane Corrosion Prevention and Control Program: Model 737-100/200. Document D6-38528, revision D. Seattle, Washington: Boeing Commercial Airplane Group. Bucci, R.B., and C.J. Warren. 1997. Material Sunstitutions for Aging Aircraft. Presentation at the DoD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, July 8–10. Bucci, R.B., R.L. Brazill, and J.R. Brockenbrough. 1986. Assessing growth of small flaws from residual strength

OCR for page 79
Aging of U.S. Air Force Aircraft: Final Report 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.

OCR for page 79
Aging of U.S. Air Force Aircraft: Final Report Hagemaier, D., and G. Kach. 1997. Eddy current detection of short cracks under installed fasteners. Materials Evaluation 55(1):25–30. Harris, C.E., J.H. Starnes, Jr., and J.C. Newman, Jr. 1995. Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structure. Pp. 139–164 in FAA-NASA Sixth International Conference on the Continued Airworthiness of Aircraft Structures, C.A. Bigelow, ed. DOT/FAA/AF-95-86. Atlantic City, N.J.: FAA Technical Center. Hart-Smith, L.J. 1974: Analysis and Design of Advanced Composite Bonded Joints. NASA-CR-2218. Washington, D.C.: National Aeronautics and Space Administration. Hegedus, C.R., S.J. Spadafora, and A.T. Eng. 1995. Organic coating technology for the protection of aircraft against corrosion. Pp. 17-1–17-10 in Corrosion Detection and Management of Advanced Airframe Materials. AGARD-CP-565. Advisory Group for Aerospace Research and Development. Neuilly-Sur Seine, France: North Atlantic Treaty Organization. Hidano, L.A., and U.G. Goranson. 1995. Inspection programs for damage tolerance—Meeting the regulatory challenge. Pp. 193–211 in Proceedings of the FAA-NASA Sixth International Conference on the Continued Airworthiness of Aircraft Structures. DOT/FAA/AR-95/86. Atlantic City, N.J.: FAA Technical Center. Hong, C.S., and K.Y. Jeng. 1985. Stress intensity factors in anisotropic sandwich plate with a part-through crack under mixed mode deformation. Engineering Fracture Mechanics 21:285–292. Howard, M., and G. Mitchell. 1997. Evaluation of Wing Skin Fastener Hidden Corrosion Damage Assessment Technologies. Presentation at the DOD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, July 8–10. Hsu, D.K., and T.C. Patton. 1993. Development of ultrasonic inspection for adhesive bonds in aging aircraft. Materials Evaluation 51(12):1390–1397. JACG (Joint Aeronautical Commanders Group). 1996. U.S. Aviation S&T Roadmap: Aviation Vision, Vol. 1. Washington, D.C.: JACG S&T Process Board. Jeans, L.L., G.C. Grimes, and H.-P. Kan. 1980. Fatigue Spectrum Sensitivity Study of Advanced Composite Materials. AFWAL-TR-80-3130. Wright-Patterson AFB, Ohio: Wright Aeronautical Laboratories. Jones, R., and R.J. Callinan. 1979. Finite element analysis of patched cracks. Journal of Structural Mechanics 7(2):107–130. Kan, H.-P. and M.M. Ratwani. 1981. Nonlinear behavior effects in cracked metal-to-composite bonded structures. Engineering Fracture Mechanics 15(1–2):123–130. Kim, J., and N. Stubbs. 1995. Damage localization accuracy as a function of model uncertainty in the I-40 bridge over the Rio Grande. Paper 2446-23 in SPIE Proceedings, Vol. 2446. Smart Structures and Materials 1995: Smart Systems for Bridges, Structures, and Highways. L.K. Matthews and N. Stubbs, eds. Bellingham, Washington: Society of Photo-Optical Instrumentation Engineers. Ko, W.L. 1978. An orthotropic sandwich plate containing a part-through crack under mixed mode deformation. Engineering Fracture Mechanics 10:15–23. Komsky, I.N., and J.D. Achenbach. 1996. Ultrasonic imaging of corrosion and fatigue cracks in multilayered airplane structures. Pp. 380–388 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. Komsky, I.N., J.D. Achenbach, G. Andrew, B. Grills, J. Register, G. Linkert, G.M. Huerto, A.L. Steinberg, M. Ashbaugh, D.G. Moore, G. Moore, and H. Weber. 1995. An ultrasonic technique to detect corrosion in DC-9 wing box from concept to field application. Materials Evaluation 53(7):848–852. Leidheiser, H., and N. Das. 1975. Penetration of hydrogen into Al exposed to water. Journal of the Electrochemical Society 122(5):640–641. Lichtenwalner, P.F., J.P. Dunne, R.S. Becker, and E.W. Baumann. 1997. Active damage interrogation system for structural health monitoring. Paper 3044-19 in SPIE Proceedings, Vol. 3044. Bellingham, Washington: Society of Photo-Optical Instrumentation Engineers. Lincoln, J.W. 1996. Aging aircraft issues in the United States Air Force. SAMPE Journal 32(5):27–33. Lincoln, J.W. 1997. Risk Assessments of Aging Aircraft. Presentation at the DOD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, July 8–10. Ma, X.P., and J.P. Wikswo. 1996. Depth selective eddy current techniques for second layer flaw detection. Pp. 401–408 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 15. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Miller, R.N. 1987. Predictive Corrosion Modeling Phase I/Task II Summary Report. AFWAL-TR-4069. Wright-Patterson AFB, Ohio: Wright Aeronautical Laboratories. Mindlin, H., B.F. Gilp, L.S. Elliott, M. Chamberlain, and T. Lynch. 1996. Corrosion in DOD Systems: Data Collection and Analysis (Phase I). MIAC Report 8. West Lafayette, Indiana: Metals Information Analysis Center (Purdue University). Mitchell, R.A., R.M. Wooley, and D.J. Chivirut. 1975. Analysis of composite reinforced cutouts and cracks. AIAA Journal 13:774-749. Moore, D. 1997. Navy Research in Aging Aircraft Technology. Presentation to the Committee on Aging of U.S. Air Force Aircraft, Washington, D.C., April 28. Moulder, J.C., M.W. Kubovich, E. Uzal, and J.H. Rose. 1995. Pulsed eddy current measurements of corrosion-induced metal loss: Theory and experiment . Pp. 2065–2072 in

OCR for page 79
Aging of U.S. Air Force Aircraft: Final Report Review of Progress in Quantitative Nondestructive Evaluation, Vol. 14. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Moulder, J.C., J.A. Bieber, W.W. Ward, and J.H. Rose. 1996. Scanned pulsed eddy current instrument for nondestructive inspection of aging aircraft. Pp. 2–13 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. Nakagawa, N. 1988. Eddy current detection methods for surface-breaking tight cracks. Pp. 245–250 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 7. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Nakagawa, N., and R.E. Beissner. 1990. Probability of tight crack detection via eddy current inspection. Pp. 893–899 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 9. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. NRC (National Research Council). 1995. Expanding the Vision of Sensor Materials. NMAB-470. National Materials Advisory Board. Washington, D.C.: National Academy Press. NRC. 1996a. New Materials for Next-Generation Commercial Transports. NMAB-476. National Materials Advisory Board. Washington, D.C.: National Academy Press. NRC. 1996b. Accelerated Aging of Materials and Structures: The Effects of Long-Term Elevated Temperature Exposure. NMAB-479. National Materials Advisory Board. Washington, D.C.: National Academy Press. NRC. 1997. Aging of U.S. Air Force Aircraft: Interim Report. Report No. NMAB 488-1. National Materials Advisory Board. Washington, D.C.: National Academy Press. NTSB (National Transportation Safety Board). 1988. Aircraft Accident Report: Aloha Airlines, Flight 243, Boeing 737-200, N73711, Near Maui, Hawaii, April 28, 1988. NTSB/AAR-89/03. Washington, D.C.: NTSB. Panhuise, V.E. 1989. Introduction. Pp. 663–665 in Metals Handbook, Volume 17: Nondestructive Evaluation and Quality Control. Metals Park, Ohio: ASM International. Park, J.H., T. Ogiso, and S.N. Atluri. 1992. Analysis of cracks in aging aircraft structures, with and without composite-patch repairs. Computational Mechanics 10:169–201. Podney, W., and J. Moulder. 1997. Electromagnetic microscope for deep pulsed eddy current inspections. Pp. 1037–1044 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 16. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Ratwani, M.M. 1996. Repair/refurbishment of military aircraft. Pp. 6-1–6-21 in Aging Combat Aircraft Fleets—Long Term Applications. AGARD-LS-206. Advisory Group for Aerospace Research and Development. Neuilly-Sur Seine, France: North Atlantic Treaty Organization. Ricker, R.E., and D.J. Duquette. 1988. The role of hydrogen in corrosion fatigue of high purity Al-Zn-Mg exposed to water vapor. Metalurgical Transactions A 19A:1775–1783. Ritchie, R.O., and J. Lankford. 1986. Small Fatigue Cracks. Warrendale, Pennsylvania: The Metallurgical Society of AIME. Rogers, L., J. Maly, I. Searle, R. Ikegami, W. Owen, R. Gordon, and D. Conley. 1997. Durability Patch: Repair and Life Extension of High Cycle Fatigue Damage on Secondary Structure of Aging Aircraft. Presentation at the DoD/FAA/NASA Conference on Aging Aircraft, Ogden, Utah, July 8–10. Rose, L.R.R. 1981. An application of inclusion analogy. International Journal on Solids and Structures 17:827–838. Rudd, J.L. 1996. USAF aging aircraft program. Pp. 1-1–1-13 in Aging Combat Aircraft Fleets—Long Term Applications. Advisory Group for Aerospace Research and Development (AGARD) Lecture Series 206. Neuilly-Sur Seine, France: North Atlantic Treaty Organization. Rummel, W.D. 1989. Applications of NDE reliability to systems. Pp. 674–688 in Metals Handbook, Vol. 17. Nondestructive Evaluation and Quality Control. Metals Park, Ohio: ASM International. SAB (Scientific Advisory Board). 1994. Report of the Ad Hoc Committee on Life Extension and Mission Enhancement for Air Force Aircraft, Vol. 1. Executive Summary. U.S. Air Force Scientific Advisory Board Report No. SAB-TR-94-01. Washington, D.C.: Department of the Air Force. SAB. 1996. Report of the Materials Degradation Panel, Ad Hoc Committee on Life Extension and Mission Enhancement for Air Force Aircraft, U.S. Air Force Scientific Advisory Board. Washington, D.C.: Department of the Air Force. Saff, C.R., and M.A. Ferman. 1986. Fatigue life analysis of fuel tank skins under combined loads. Pp. 277–290 in Case Histories Involving Fatigue and Fracture Mechanics. ASTM-STP-918. Philadelphia, Pennsylvania: American Society for Testing and Materials. Schmerr, L.W., and D.O. Thompson. 1994. NDE and design—a unified life-cycle engineering approach. Pp. 2183–2190 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 13. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Sethuraman, R., and S.K. Mathi. 1989. Determination of mixed mode stress intensity factors for a crack-stiffened panel. Engineering Fracture Mechanics 33:355–369. Smith, S.W., and J.R. Scully. 1996. Hydrogen trapping and its correlation to the hydrogen embrittlement susceptibility of Al-Li-Cu-Zr alloys. Pp. 131–141 in Hydrogen Effects in Materials. A.W. Thompson and N.R. Moody, eds. Warrendale, Pennsylvania: The Minerals, Metals, and Materials Society.

OCR for page 79
Aging of U.S. Air Force Aircraft: Final Report Spencer, F., and D. Schurman. 1995. Reliability Assessment of Airline Inspection Facilities: Vol. 3. Results of an Eddy Current Inspection Reliability Experiment. DOT/FAA/CT-92/12. Atlantic City, N.J.: FAA Technical Center. SPIE (Society of Photo-Optical Instrumentation Engineers). 1996. Proceedings of NDE of Aging Aircraft, Airports, and Aerospace Hardware, Vol. 2945. R.D. Rempt and A. Broz, eds. Bellingham, Washington: SPIE. Spiedel, M.O. 1975. Stress corrosion cracking of aluminum alloys. Metallurgical Transactions A 6A:631–651. Sprowls, D.O., R.J. Bucci, B.M. Ponchel, R.L. Brazill, and P.E. Bretz. 1984. A Study of Environmental Characterization of Conventional and Advanced Aluminum Alloys for Selection and Design. Phase II—The Breaking Load Test Method. NASA-CR-172387. Washington, D.C.: National Aeronautics and Space Administration. Syed, H.I., W.P. Winfree, K.E. Cramer, and D.A. Howell. 1995. Thermographic detection of corrosion in aircraft skins. Pp. 2035–2041 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 14. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Tarn, J.Q., and K.L. Shek. 1991. Analysis of crack plates with a bonded patch. Engineering Fracture Mechanics 40:1055–1065. Taylor, S.R., N.P. Cella, G.E. Stoner, R.G. Buchheit, and L.P. Montes. 1997. Environmentally Compliant Corrosion Resistant and Electrically Conductive Inorganic Coatings for Aluminum Alloys. DARPA Progress Report, contract no. F49620-96-0305. Washington, D.C.: Defense Advanced Research Projects Agency. Thome, D.K., G.L. Fitzpatrick, R.L. Skaugset, and W.C.L. Shih. 1996. Aircraft corrosion and crack inspection using advanced magneto-optic imaging technology. Pp. 365–373 in SPIE Proceedings, Vol. 2945. NDE of Aging Aircraft, Airports, and Aerospace Hardware. Rempt and A. Broz, eds. Bellingham, Washington: Society of Photo-Optical Instrumentation Engineers. Thompson, D.O., and L.W. Schmerr, Jr. 1993. The role of modeling in the determination of probability of detection. Pp. 285–301 in Advances in Signal Processing for Nondestructive Evaluation of Materials. X.P.V. Moldague, ed. Boston: Kluwer Academic Publishers. Ting, J., T. Jensen, and J. Gray. 1993. Using energy dispersive x-ray measurements for quantitative determination of materials loss due to corrosion. Pp. 1963–1969 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 12. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Vosteen, L.F., and R.N. Hadcock. 1994. Composite Chronicles: A Study of the Lessons Learned in the Development, Production, and Service of Composite Structures. NASA-CR-4620. Washington, D.C.: National Aeronautics and Space Administration. Walter, P. 1995. The FAA's aging aircraft nondestructive inspection validation center at Sandia National Laboratories: An introduction. Materials Evaluation 53(7):799–802. Whitehead, R.S., H. Kan, R. Cordero, and E. Saether. 1986. Certification Testing Methodology for Composite Structures. Final Report, March 1984-December 1985. Warminster, Pennsylvania: Naval Air Development Center. Wincheski, B., J.R. Fulton, S. Nath, M. Namburg, and J.W. Simpson. 1994. Self-nulling eddy current probe for surface and subsurface flaw detection. Materials Evaluation 52(1):22–26. Wincheski, B., R. Todhunter, and J. Simpson. 1997. A new instrument for the detection of cracks under airframe rivets. Pp. 2113–2120 in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 16. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press. Winfree, W.P. 1996. New nondestructive techniques for inspection of aircraft structures. Pp. 2–13 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. Xu, J., R. Wallingford, T. Jensen, and J. Gray. 1994. Recent developments in the x-ray simulation code: XRSIM. Pp. 557–562 in Review of Progress in Quantitative Nondestructive Evaluation, Vo.. 13. D.O. Thompson and D.E. Chimenti, eds. New York: Plenum Press.

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