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| Session 1: Engineered Residual Stresses | ||||
| Location: Mercer A & B (Hilton Seattle Airport & Conference Center) | ||||
| (Please check final room assignments on-site). | ||||
| Session Description: | ||||
| Session Chair: | Dr. James E. Pillars The Boeing Company, Seattle, WA | |||
| 8:30 AM | WAJ1.1 | High Throughput Production Laser Peening: A Very Successful Technology Transfer | ||
| 9:00 AM | WAJ1.2 | Improved Damage Tolerance in Ti-6Al-4V Aero Engine Blades and Vanes Using Leading Edge Residual Compression in Design | ||
| 9:30 AM | WAJ1.3 | Understanding Material Performance Through Determination of Spatial Variations of Residual Stress | ||
| 10:00 AM | Break | |||
| 10:30 AM | WAJ1.4 | The Effects of Laser Peening on the Fatigue Performance of Aerospace Structural Alloys | ||
| 11:00 AM | WAJ1.5 | Laser Shock Peening: Process Overview and Current Status | ||
| 11:30 AM | WAJ1.6 | Fretting Fatigue of Laser Peened Ti-6Al-4V | ||