Validation of Fatigue Crack Growth Rate Constant with Loading Parameters for 6063-T6 Aluminum AlloyApril 25, 2013Validation of Fatigue Crack Growth Rate Constant with Loading Parameters for 6063-T6 Aluminum Alloy, By-Shivangi Kaushal -2013.
Review on Fatigue crack growth and finite element methodApril 4, 2013“Review on Fatigue crack growth and finite element method, Nirpesh Vikram, Dr. Raghuvir Kumar, International Journal of Science & Engineering Research, Vol.4, Issue 4, April 2013, ISSN [...]