Mo.5.A.2 IMPACT DAMAGE DETECTION IN GRAPHENE DOPED CFRP LAMINATES
Mo.4.A.6 POSITIONING NDT SENSORS WITH A MOBILE ROBOT FOR EFFICIENT AIRCRAFT INSPECTIONS
Mo.4.A.5 A ROUND ROBIN TEST OF FLASH THERMOGRAPHY OF CFRP STRUCTURES
Mo.4.A.4 SIMULATION OF STRUCTURAL DAMAGE AND ITS DETECTION BY METHOD OF ELECTROMECHANICAL IMPEDANCE
Mo.4.A.2 IN-SERVICE STRUCTURAL HEALTH MONITORING TECHNIQUE FOR LARGE AEROSPACE COMPOSITE STRUCTURES
Mo.4.A.1 AUTONOMOUS WIRELESS ACOUSTIC SENSORS FOR AERONAUTICAL SHM APPLICATIONS
Mo.3.A.6 HIGH RESOLUTION NDT&E OF CARBON FIBER REINFORCED COMPOSITES
Mo.3.A.5 NDE OF DISSIMILAR JOINTS USING ULTRASONICS AND X-RAY TOMOGRAPHY
Mo.3.A.4 ULTRASONIC TRACKING OF PLY DROPS IN COMPOSITE LAMINATES ~ EXPERIMENTAL VALIDATION
Mo.3.A.3 COMPARATIVE STUDY OF DIFFERENT NONDESTRUCTIVE TESTING METHODS TO DETECT DAMAGES IN GRIP
Mo.3.A.2 LASER ULTRASONICS INSPECTIONS OF AERONAUTICAL COMPONENTS VALIDATED BY COMPUTED TOMOGRAPHY
Mo.3.A.1 A STATE SPACE APPROACH FOR THE NON-DESTRUCTIVE EVALUATION OF CFRP WITH ULTRASONIC
Mo.1.A.1 INVITED LECTURE: RECENT AND FUTURE ENHANCEMENTS IN NDI FOR AIRCRAFT STRUCTURES