Titlebook: Structural Integrity of Aging Airplanes; S. N. Atluri (J. C. Hunsaker Visiting Professor),S Conference proceedings 1991 Springer-Verlag Be

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A Damage Tolerance Approach for Management of Aging Gas Turbine Engines,age Tolerance Philosophy and implementation of a Fracture Control Program has been an integral part of the USAF turbine engine development process since 1978. It has been applied to new engine programs as part of the USAF’s Engine Structural Integrity Program (ENSIP) described in military standard 1

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Aging Jet Transport Structural Evaluation Programs, age of the world airline jet transport fleet has increased from 8 to 12 years since 1980. Standard Boeing practices to ensure continuing airplane structural integrity include inspection and overhaul recommendations contained in maintenance manuals 2nd service bulletins. As airplanes exceed their ec

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,The Aloha Airlines Accident — A New Era for Aging Aircraft,fferent about this occurrence is that in the past it has usually been the high fatality spectacular catastrophic accidents that have worked as the catalyst for change. High visibility aviation accidents with great loss of life would serve as the trigger for stampeding the government and industry int

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Applications of Advanced Fracture Mechanics to Fuselage,cial aircraft nearing their design life targets. Consequently, to assure the safety of aircraft that have accumulated large numbers of flights, flight hours and years in service requires inspection procedures that are based on the possibility that MSD may be present For inspections of aircraft compo

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