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Recent advances in the modelling of crack growth under fatigue loading conditionsFatigue crack growth associated with cyclic (secondary) plastic flow near a crack front is modelled using an incremental formulation. A new description of threshold behaviour under small load cycles is included. Quasi-static crack extension under high load excursions is described using an incremental formulation of the R-(crack growth resistance)- curve concept. The integration of the equations is discussed. For constant amplitude load cycles the results will be compared with existing crack growth laws. It will be shown that the model also properly describes interaction effects of fatigue crack growth and quasi-static crack extension. To evaluate the more general applicability the model is included in the NASGRO computer code for damage tolerance analysis. For this purpose the NASGRO program was provided with the CORPUS and the STRIP-YIELD models for computation of the crack opening load levels. The implementation is discussed and recent results of the verification are presented.
Document ID
19950008064
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dekoning, A. U.
(National Aerospace Lab. Amsterdam, Netherlands)
Tenhoeve, H. J.
(National Aerospace Lab. Amsterdam, Netherlands)
Henriksen, T. K.
(National Aerospace Lab. Amsterdam, Netherlands)
Date Acquired
September 6, 2013
Publication Date
September 1, 1994
Publication Information
Publication: NASA. Langley Research Center, FAA(NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance
Subject Category
Structural Mechanics
Accession Number
95N14478
Funding Number(s)
CONTRACT_GRANT: NIVR-1823
CONTRACT_GRANT: NIVR-9691
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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