Validation of Fatigue Crack Growth Rate Constant with Loading Parameters for 6063-T6 Aluminum Alloy2013-04-252018-07-25https://bbdu.ac.in/wp-content/uploads/2018/10/bbd-logo-3.pngBBDUhttps://bbdu.ac.in/wp-content/uploads/2018/10/bbd-logo-3.png200px200px
Validation of Fatigue Crack Growth Rate Constant with Loading Parameters for 6063-T6 Aluminum Alloy, By-Shivangi Kaushal -2013.