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Aging of U.S. Air Force Aircraft: Final Report (1997)
National Materials Advisory Board (NMAB)

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. "References." Aging of U.S. Air Force Aircraft: Final Report. Washington, DC: The National Academies Press, 1997.

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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.

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