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Simulation of Fatigue Crack Initiation at Corrosion Pits With EDM NotchesUniaxial fatigue tests were conducted to compare the fatigue life of laboratory produced corrosion pits, similar to those observed in the shuttle main landing gear wheel bolt-hole, and an electro-discharged-machined (EDM) flaw. EDM Jaws are used to simulate corrosion pits during shuttle wheel (dynamometer) testing. The aluminum alloy, (AA 7050) laboratory fatigue tests were conducted to simulate the local stress level contained in the wheel bolt-hole. Under this high local stress condition, the EDM notch produced a fatigue life similar to test specimens containing corrosion pits of similar size. Based on the laboratory fatigue test results, the EDM Jaw (semi-circular disc shaped) produces a local stress state similar to corrosion pits and can be used to simulate a corrosion pit during the shuttle wheel dynamometer tests.
Document ID
20030032270
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Smith, Stephen W.
(NASA Langley Research Center Hampton, VA, United States)
Newman, John A.
(Army Research Lab. Hampton, VA, United States)
Piascik, Robert S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2003
Subject Category
Quality Assurance And Reliability
Report/Patent Number
NASA/TM-2003-212166
L-18262
NAS 1.15:212166
AFL-TR-2927
Funding Number(s)
CONTRACT_GRANT: RTOP 762-60-61-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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