Structural health monitoring R&D at the “European Research Establishments in Aeronautics” (EREA)

A description of the compared activities in structural health monitoring of the seven main research establishments in aeronautics and aerospace sciences in Europe, grouped in the EREA association, is made, with emphasis on the more recent and interesting results obtained in this field.

[1]  Daniel L. Osmont,et al.  Active health system based on wavelet transform analysis of diffracted Lamb waves , 2000, Symposium on Applied Photonics.

[2]  Klas Levin,et al.  Behavior of an embedded piezoceramic transducer for Lamb wave generation in mechanical loading , 2000, Smart Structures.

[3]  Klas Levin,et al.  Location of Embedded Fiber Optic Sensors for Minimized Impact Vulnerability , 1999 .

[4]  Klas Levin,et al.  Structural integrity of composites with embedded piezoelectric ceramic transducers , 1999, Smart Structures.

[5]  Klas Levin,et al.  Vulnerability of embedded EFPI-sensors to low-energy impacts , 1997 .

[6]  Moulin,et al.  Modeling of lamb waves generated by integrated transducers in composite plates using a coupled finite element-normal modes expansion method , 2000, The Journal of the Acoustical Society of America.

[7]  Stephan Kaiser,et al.  Structural dynamic health monitoring of adaptive CFRP structures , 1999, Smart Structures.

[8]  Emmanuel Moulin,et al.  Piezoelectric transducer embedded in a composite plate: Application to Lamb wave generation , 1997 .

[9]  M. Dupont,et al.  Comparison between Non-Destructive Evaluation Techniques and Integrated Fiber Optic Health Monitoring Systems for Composite Sandwich Structures , 2000 .

[10]  Daniel L. Osmont,et al.  Laser-generated Lamb waves in carbon/epoxy composite structures using an embedded fiber optic delivery system , 2000, Smart Structures.

[11]  Daniel L. Osmont,et al.  Piezoelectric transducer network for dual-mode (active/passive) detection, localization, and evaluation of impact damages in carbon/epoxy composite plates , 2000, Symposium on Applied Photonics.

[12]  Arne Skontorp,et al.  Static fatigue life of silica optical fibers and the significance of fiber coating and handling , 2001, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[13]  Marc Pernice,et al.  Integration of optical fibers and piezoelectric ceramics in composite materials , 1996, Other Conferences.

[14]  A. Skontorp.  Structural Integrity of Quasi-Isotropic Composite Laminates with Embedded Optical Fibers , 2000 .

[15]  David Devillers,et al.  Interaction of Lamb waves with defects in composite sandwich structures , 2000 .

[16]  Frédéric Taillade,et al.  Shearographic visualization of lamb waves in carbon epoxy plates interaction with delaminations , 2000 .

[17]  Anders Sjogren,et al.  Connection of optical fibers embedded in aircraft composite components , 2000, Smart Structures.

[18]  M. Dupont,et al.  Damage detection in a radome sandwich material with embedded fiber optic sensors , 2000 .

[19]  C. Delebarre,et al.  Comparison between flat multi-element array device and oblique incidence transducers for Lamb waves generation: application for embedment in composite material , 1996, Other Conferences.

[20]  Antonello Cutolo,et al.  An optoelectronic sensor for cure monitoring in thermoset-based composites , 2000 .

[21]  J. Melcher.  Synthesis of Optimized Adaptive Digital Filters for System Identification and Vibration Control. , 1991 .

[22]  Arne Skontorp,et al.  Strength and failure mechanisms of polyimide-coated optical fibers , 2000, Smart Structures.

[23]  Michel B. Lemistre,et al.  Electromagnetic Structural Health Monitoring for Composite Materials , 2001 .

[24]  Antonello Cutolo,et al.  Integrated fiber optic sensing system for in-situ characterization of the curing process of thermoset-based composites , 2001, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[25]  M. Lemistre,et al.  Damage localization in composite plates using wavelet transform processing on Lamb wave signals , 1999 .