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/2024/09/bbdu-logo.gifBBDUhttps://bbdu.ac.in/wp-content/uploads/2024/09/bbdu-logo.gif200px200px
Validation of Fatigue Crack Growth Rate Constant with Loading Parameters for 6063-T6 Aluminum Alloy, By-Shivangi Kaushal -2013.