Structures / American Institute of Aeronautics and Astronautics ; Volume 2 of 3
Structures / American Institute of Aeronautics and Astronautics ; Volume 3 of 3
Structures / American Institute of Aeronautics and Astronautics ; Volume 1 of 3
Nichtlineare Auslegung abgestrebter Transportflugzeugflügel
Aircraft structures : mechanics, design, and maintenance
Long-life design and test technology of typical aircraft structures
Supersonic business jets in preliminary aircraft design
Supersonic business jets in preliminary aircraft design
We.5.A.1 GEOMETRIC CALIBRATION FOR THERMOGRAPHY CAMERAS
We.2.A.6 NUTHIC: NON-CONTACT ULTRASOUND INSPECTION MACHINE OF HIGHLY INTEGRATED COMPOSITE PARTS
Tu.2.A.5 DESIGN OF A STRUCTURAL HEALTH MONITORING SYSTEM FOR A DAMAGE TOLERANCE FUSELAGE COMPONENT
We.5.A.4 EDDY CURRENT TESTING WITH HIGH-SPATIAL RESOLUTION PROBES USING MR ARRAYS AS RECEIVER
We.4.A.5 NON-DESTRUCTIVE MATERIAL TESTING WITH INFRARED THERMOGRAPHY
Mo.3.A.1 A STATE SPACE APPROACH FOR THE NON-DESTRUCTIVE EVALUATION OF CFRP WITH ULTRASONIC
Tu.1.A.4 COMPOSITES SURFACE STATE ASSESSMENT BY LIF METHOD
We.2.A.5 VISUALISATION OF ULTRASONIC TESTING DATA USING AUGMENTED REALITY
We.4.A.3 IT SUPPORT OF NDE AND SHM WITH APPLICATION OF THE METAL MAGNETIC MEMORY METHOD
We.4.A.2 SMART MOBILE WORKER, THE SOLUTION TO IMPROVE PRODUCTIVITY
Mo.1.A.1 INVITED LECTURE: RECENT AND FUTURE ENHANCEMENTS IN NDI FOR AIRCRAFT STRUCTURES
Mo.5.A.2 IMPACT DAMAGE DETECTION IN GRAPHENE DOPED CFRP LAMINATES
Tu.3.A.5 DATA ASSIMILATION FOR MONITORING RESIN TRANSFER MOLDING OF COMPOSITE MATERIALS
Mo.4.A.1 AUTONOMOUS WIRELESS ACOUSTIC SENSORS FOR AERONAUTICAL SHM APPLICATIONS
Mo.3.A.5 NDE OF DISSIMILAR JOINTS USING ULTRASONICS AND X-RAY TOMOGRAPHY