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IssuesArchive of Issues2011-6pp.828-838

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N.G. Bourago, A.B. Zhuravlev, and I.S. Nikitin, "Models of Multiaxial Fatigue Fracture and Service Life Estimation of Structural Elements," Mech. Solids. 46 (6), 828-838 (2011)
Year 2011 Volume 46 Number 6 Pages 828-838
DOI 10.3103/S0025654411060033
Title Models of Multiaxial Fatigue Fracture and Service Life Estimation of Structural Elements
Author(s) N.G. Bourago (Ishlinsky Institute for Problems in Mechanics, Russian Academy of Sciences, pr-t Vernadskogo 101, str.&nsbp;1, Moscow, 119526 Russia, burago@ipmnet.ru)
A.B. Zhuravlev (Joint Institute for High Temperatures, Russian Academy of Sciences, Izhorskaya 13-2, Moscow, 125412 Russia)
I.S. Nikitin (Moscow State Aviation Technological University, Orshanskaya 3, Moscow, 121552 Russia, i_nikitin@list.ru)
Abstract We study criteria and models of multiaxial fracture under the conditions of low-cycle fatigue (LCF). The model parameters are determined by using the data of uniaxial fatigue tests for different coefficients of the cycle asymmetry. A procedure for calculating the stress state of the compressor disk in a gas turbine engine (GTE) in the flight cycle of loading is outlined. The calculated stress state and models of multiaxial fatigue fracture are used to estimate the service life of the compressor disk. The results are compared with the observational data collected during the operation.
Keywords multiaxial fatigue fracture model, service life estimation, stress concentration, centrifugal load, aerodynamic load
References
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Received 20 July 2011
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