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Session 2: Material and Structural State Awareness
Location: Room 302 (Dayton Convention Center )
(Please check final room assignments on-site).
Session Description:
Session Chair:	Mr. Eric Lindgren Air Force Research Laboratory, Wright Patterson Air Force Base, OH
1:30 PM	SSP2.1		Ultrasonic Sensing for Structural State Awareness of Fastener Hole Fatigue Cracks
2:00 PM	SSP2.2		Vibration and on-Line Oil Debris Sensor Fusion for Aircraft Engine Bearing Prognosis
2:30 PM	SSP2.3		Direct Sensing of the Composite Materials Elastic Modulus
3:00 PM			Break
3:30 PM	SSP2.4		Advanced Nonlinear Vibration Analysis for Next-Generation Crack Propagation Algorithms
4:00 PM	SSP2.5		Automated Fatigue Test Monitoring and Damage Evolution Tracking for Prognosis in Support of Condition Based Maintenance Decisions – Part I: Fatigue Tests
4:30 PM	SSP2.6		Automated Fatigue Test Monitoring and Damage Evolution Tracking for Prognosis in Support of Condition Based Maintenance Decisions – Part II: Prognosis
5:00 PM	SSP2.7		Digtial Radiography for the Aerospace Industry