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| Session 1: High Strength 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 | |||
| 8:30 AM | LAT1.1 | Latest Generation of Al-Li Plate Alloys Developed by Alcan Aerospace | ||
| 9:00 AM | LAT1.2 | Kaiser Aluminum 6019 for Aerospace Sheet and Plate Applications | ||
| 9:30 AM | LAT1.3 | Improved Aluminium Sheet and Plate Alloys for Aircraft Fuselage, Wing and Integrated Structures | ||
| 10:00 AM | Break | |||
| 10:30 AM | LAT1.4 | Concepts and Concept Validation for Advanced Metallic Structures | ||
| 11:00 AM | LAT1.5 | Modeling of 7081 Plate Applications for High Performance - Cost Efficient Aircraft Structures | ||