High Temperature Dwell Fatigue Crack Growth in Cold-Worked and Direct-Aged 718PlusTM
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-030-51834-9_58
Reference16 articles.
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2. M. Cemal, S. Cevik, Y. Uzunonat, F. Diltemiz, ALLVAC 718 PlusTM Superalloy for Aircraft Engine Applications, in: Recent Adv. Aircr. Technol., 2012. https://doi.org/10.5772/38433.
3. B.J. Bond, R.L. Kennedy, Evaluation of Allvac® 718PlusTM alloy in the cold worked and heat treated condition, in: Proc. Int. Symp. Superalloys Var. Deriv., 2005. https://doi.org/10.7449/2005/superalloys_2005_203_211.
4. W. Li, D. Terret, E. McDevitt, S. Ndoye, S. Gardner, Development of ati 718Plus® for high temperature high strength fastener applications, in: 8th Int. Symp. Superalloy 718 Deriv. 2014, 2014. https://doi.org/10.1002/9781119016854.ch40.
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