Author:
Kant Chandra,Harmain G. A.
Publisher
Springer Nature Singapore
Reference37 articles.
1. Lee EU, Glinka G, Vasudevan AK, Iyyer N, Phan ND (2009) Fatigue of 7075–T651 aluminum alloy under constant and variable amplitude loadings. Int J Fatigue 31:1858–1864. https://doi.org/10.1016/j.ijfatigue.2008.11.013
2. De Jong JB, Schütz D, Lowak H, Schijve J (1973) A standardized load sequence for flight simulation tests on transport aircraft wing structures. NLR-TR 73029 U, LBF Bericht FB-106
3. Wahab MA, Rohrsheim GR, Park JH (2004) Experimental study on the influence of overload induced residual stress field on fatigue crack growth in aluminium alloy. J Mater Process Technol 153–154:945–951. https://doi.org/10.1016/j.jmatprotec.2004.04.348
4. Kant C, Harmain GA (2021) An investigation of constant amplitude loaded fatigue crack propagation of virgin and pre- strained aluminium alloy. In: International conference on advanced manufacturing and materials processing, pp 1–14
5. Wheeler OE (1972) Spectrum loading and crack growth. J Fluids Eng Trans ASME 94:181–186. https://doi.org/10.1115/1.3425362
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