Tu.2.A - Aeronautics
|
|
Tu.2.A.1
|
Onboard - SHM for Life Time Prediction and Damage Detection on Aircraft Structure Using Fibre Optical Sensor and LAMB Wave Technology 
|
|
|
U. Berger, IABG, Ottobrunn, Germany
|
|
Tu.2.A.2
|
Flight Load Monitoring of Aerospace Structures Using a Fibre Bragg Grating System
|
|
|
B. Rocha, A. Beltempo, M. Martinez, R. Rutledge, M. Yanishevsky, National Research Council Canada, Ottawa, Canada
|
|
Tu.2.A.3
|
Energy Harvesting, Wireless, Non-Contacting Slip Ring for Rotorcraft
|
|
|
S. Arms, M. Hamel, M. Hogan, C.P. Townsend, MicroStrain, Williston, USA
N. Phan, R. Semidey, NAVAIR, Patuxent River, USA
|
|
Tu.2.A.4
|
Damage Detection in a Helicopter Composite Tailboom by Mode Conversion of Lamb Waves
|
|
|
W. Hillger, A. Szewieczek, DLR, Braunschweig, Germany
|