Tu.2.A.6 SIMULATION OF GUIDED WAVES SHM SYSTEM IN CIVA PLATFORM
Mo.3.A.3 COMPARATIVE STUDY OF DIFFERENT NONDESTRUCTIVE TESTING METHODS TO DETECT DAMAGES IN GRIP
Tu.2.A.2 APPLICATION OF THE FATIGUE CRACK OPENING/CLOSING EFFECT FOR AIRCRAFT SHM
7th International Symposium on NDT in Aerospace 2015 : 16-18 November 2015 in Bremen, Germany
Mo.4.A.5 A ROUND ROBIN TEST OF FLASH THERMOGRAPHY OF CFRP STRUCTURES
Mo.3.A.2 LASER ULTRASONICS INSPECTIONS OF AERONAUTICAL COMPONENTS VALIDATED BY COMPUTED TOMOGRAPHY
Tu.1.A.4 COMPOSITES SURFACE STATE ASSESSMENT BY LIF METHOD
We.2.A.5 VISUALISATION OF ULTRASONIC TESTING DATA USING AUGMENTED REALITY
We.5.A.5 LASER SPOT THERMOGRAPHY FOR CRACK DETECTION IN ALUMINUM STRUCTURES
We.5.A.2 THICKNESS MEASUREMENT OF MULITLAYER COATING USING TERAHERTZ TECHNIQUES
We.4.A.6 LASER ULTRASONIC MODELLING FOR NDT APPLICATIONS
We.3.A.8 THE FUTURE OF ON-WING-INSPECTION
We.3.A.6 INSPECTION OF WELDS WITH IMPULSE ACOUSTIC MICROSCOPY
Tu.1.A.5 NEAR-INFRARED OPTICAL COHERENCE TOMOGRAPHY FOR THE INSPECTION OF FIBER COMPOSITES