6th European Workshop on Structural Health Monitoring > Proceedings > Tu.4.A

Tu.4.A - Aeronautics
Tu.4.A.1	Helicopter HUMS & The Path to CBM
	F. Hoffmann, Eurocopter Deutschland, München, Germany
Tu.4.A.2	Capability Study of Embedded Ultrasonic Transducer Microsystems for SHM Applications in Airplane Composite Structures
	F. Schubert, Fraunhofer IZFP, Dresden, Germany M. Franke, Cotesa, Mittweida, Germany G. Lautenschlaeger, N. Meyendorf, M. Röllig, Fraunhofer IZFP, Dresden, Germany B. Boehme, TU Dresden, Germany
Tu.4.A.3	Hierarchical Sensing System Combining Optical Fiber Network and Distributed Built-In CVM Sensors: Delamination Monitoring of CFRP Structure
	S. Minakuchi, H. Banshoya, S. Ii, N. Takeda, The University of Tokyo, Kashiwa-shi, Japan
Tu.4.A.4	Evaluation of Flight Data from an Airworthy Structural Health Monitoring System Integrally Embedded in an Unmanned Air Vehicle
	I. Kressel, IAI Israel Aerospace Industries, Ben Gurion Intl. Airport, Israel A.C.R. Pillai, M. Prasad, Aeronautical Development Establishment, Bangalore, India J. Balter, P. Guedj, IAI Israel Aerospace Industries, Ben Gurion Intl. Airport, Israel N. Gupta, A. Joseph, R. Sundaram, National Aerospace Labs, Bangalore, India Y. Botsev, N. Gorbatov, A. Handelman, M. Tur, Tel-Aviv University, Israel

Tu.4.A - Aeronautics