共 50 条
- [1] Strength of 2024-T3 aluminum panels with multiple site damage JOURNAL OF AIRCRAFT, 2000, 37 (02): : 325 - 331
- [2] Strength of stiffened 2024-T3 aluminum panels with multiple site damage JOURNAL OF AIRCRAFT, 2001, 38 (04): : 764 - 768
- [3] Linkup strength of 2024-T3 bolted lap joint panels with multiple-site damage JOURNAL OF AIRCRAFT, 2004, 41 (02): : 359 - 364
- [5] Link-up strength of 2524-T3 and 2024-T3 aluminum panels with multiple site damage JOURNAL OF AIRCRAFT, 2005, 42 (02): : 535 - 541
- [8] Strength of stiffened 2024-T3 aluminum panels with multiple site damage (vol 38, pg 764, 2001) JOURNAL OF AIRCRAFT, 2002, 39 (01): : 192 - 192
- [9] Effect of aging time and temperature on exfoliation corrosion of aluminum alloys 2024-T3 and 7075-T6 MATERIALS AND CORROSION-WERKSTOFFE UND KORROSION, 2007, 58 (05): : 345 - 347