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| Session 2: Damage Tolerant Aluminum Alloy Airframe Applications | ||||
| Location: Room 345 (Baltimore Convention Center) | ||||
| (Please check final room assignments on-site). | ||||
| Session Description: | ||||
| Session Chair: | Dr. David Chellman Lockheed Martin Aeronautical Systems, Marrietta, GA | |||
| 1:30 PM | LAT2.1 | Temperature Effects on the Microstructure of an Aerospace Aluminum Alloy | ||
| 2:00 PM | LAT2.2 | Advanced Metallic Frames for Future Metallic Fuselage | ||
| 2:30 PM | LAT2.3 | Latest Alloy Development Activities at Universal Alloy Corporation | ||
| 3:00 PM | Break | |||
| 3:30 PM | LAT2.4 | Elevated Temperature Performance of 2099-T83 Extruded Products | ||
| 4:00 PM | LAT2.5 | Status of New Flat Rolled Products at Alcoa | ||
| 4:30 PM | LAT2.6 | Development of Corrosion Resistant Alloys, Tempers and Testing Methodologies at Alcoa | ||