Structural Damage Monitoring of a Composite Wing Using Multiple Types of Sensors

Chan Yik Park; Chang Min Cho; Seung Moon Jun

doi:10.4028/www.scientific.net/AMR.123-125.907

Paper Titles

Damage Detection of Sandwich Structure Using Time Domain Reflectometry
p.891

Detection of Impact Location for Composite Stiffened Panel Using FBG Sensors
p.895

Determination of Vibration Source Locations in Laminated Composite Plates Using Lamb Wave Analysis
p.899

Development of Sensor Integrated Composite Wing Structure
p.903

Structural Damage Monitoring of a Composite Wing Using Multiple Types of Sensors
p.907

Temperature Independent Delamination Detection Using Data Normalization
p.911

Ultrasonic Inspection of Fiber Reinforced Cement Based Composites after their Exposure to Fire Conditions
p.915

Degradation of Volatile Acetone by a Photocatalytic Reactor with TiO₂ Coated Sieve
p.919

Photosensitization of Dye/TiO₂ Thin Films by Using Natural Dye of TCPP
p.923

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 123-125Structural Damage Monitoring of a Composite Wing...

Structural Damage Monitoring of a Composite Wing Using Multiple Types of Sensors

Abstract:

This paper outlines an ongoing SHM project called KASHMOS where the damage detection in composite wing structures using multiple sensors is investigated. The test bed is a composite UAV wing section and the ground structural tests are being performed to evaluate developed systems. Different kinds of damage modes in prearranged areas are intentionally induced. Optical fiber sensors, piezo-electric active sensors and Q-switched pulse lasers are utilized for detecting the damage and monitoring the integrity of the wing structure. Strain-based, impedance-based, and ultrasonic-wave-based damage monitoring methods are studied. Although this investigation is based on the ground tests, the operation concepts for the onboard system as well as the ground system are also considered.

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Periodical:

Advanced Materials Research (Volumes 123-125)

Pages:

907-910

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.123-125.907

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Online since:

August 2010

Authors:

Chan Yik Park, Chang Min Cho, Seung Moon Jun

Keywords:

Composite, Damage Detection, Structural Health Monitoring (SHM), Structure, Wing

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