Strain and damage monitoring in CFRP fuselage panels using fiber Bragg grating sensors. Part I: Design, manufacturing and impact testing-Reference-Cited by-同舟云学术

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Strain and damage monitoring in CFRP fuselage panels using fiber Bragg grating sensors. Part I: Design, manufacturing and impact testing

Published:2014-01 Issue: Volume:107 Page:726-736
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Tserpes K.I.,Karachalios V.,Giannopoulos I.,Prentzias V.,Ruzek R.

Funder

European Community’s Seventh Framework Programme

Clean Sky Joint Technology Initiative

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference27 articles.

1. Continuous arbitrary strain profile measurements with fiber Bragg gratings;Huang;Smart Mater Struct,1998

2. Optical and acoustic damage detection in laminated CFRP composite materials;Rippert;Composite Sci Technol,2000

3. Strain monitoring in FRP laminates and concrete beams using FBG sensors;Lau;Composite. Struct,2001

4. Buckling behavior monitoring of composite wing box model using fiber Bragg grating sensor system;Hong;Proc SPIE,2001

5. Health monitoring of composite repairs and joints using optical fibers;Jones;Composite. Struct,2002

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