Optical Sensing of the Fatigue Damage State of CFRP under Realistic Aeronautical Load Sequences

We present an optical sensing methodology to estimate the fatigue damage state of structures made of carbon fiber reinforced polymer (CFRP), by measuring variations on the surface roughness. Variable amplitude loads (VAL), which represent realistic loads during aeronautical missions of fighter aircr...

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Main Authors: Pablo Zuluaga-Ramírez, Álvaro Arconada, Malte Frövel, Tomás Belenguer, Félix Salazar
Format: Article
Language:English
Published: MDPI AG 2015-03-01
Series:Sensors
Subjects:
Online Access:http://www.mdpi.com/1424-8220/15/3/5710
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author Pablo Zuluaga-Ramírez
Álvaro Arconada
Malte Frövel
Tomás Belenguer
Félix Salazar
author_facet Pablo Zuluaga-Ramírez
Álvaro Arconada
Malte Frövel
Tomás Belenguer
Félix Salazar
author_sort Pablo Zuluaga-Ramírez
collection DOAJ
description We present an optical sensing methodology to estimate the fatigue damage state of structures made of carbon fiber reinforced polymer (CFRP), by measuring variations on the surface roughness. Variable amplitude loads (VAL), which represent realistic loads during aeronautical missions of fighter aircraft (FALSTAFF) have been applied to coupons until failure. Stiffness degradation and surface roughness variations have been measured during the life of the coupons obtaining a Pearson correlation of 0.75 between both variables. The data were compared with a previous study for Constant Amplitude Load (CAL) obtaining similar results. Conclusions suggest that the surface roughness measured in strategic zones is a useful technique for structural health monitoring of CFRP structures, and that it is independent of the type of load applied. Surface roughness can be measured in the field by optical techniques such as speckle, confocal perfilometers and interferometry, among others.
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spelling doaj.art-fe49fd56e3b64815b79e1f456f3784e12022-12-22T04:22:20ZengMDPI AGSensors1424-82202015-03-011535710572110.3390/s150305710s150305710Optical Sensing of the Fatigue Damage State of CFRP under Realistic Aeronautical Load SequencesPablo Zuluaga-Ramírez0Álvaro Arconada1Malte Frövel2Tomás Belenguer3Félix Salazar4Instituto Nacional de Técnica Aeroespacial (INTA), Carretera de Ajalvir Km 4, 28850 Torrejón de Ardoz, SpainDepartment of Applied Physics, ETSI Minas, Universidad Politécnica de Madrid, C/Ríos Rosas 21, 28003 Madrid, SpainInstituto Nacional de Técnica Aeroespacial (INTA), Carretera de Ajalvir Km 4, 28850 Torrejón de Ardoz, SpainInstituto Nacional de Técnica Aeroespacial (INTA), Carretera de Ajalvir Km 4, 28850 Torrejón de Ardoz, SpainDepartment of Applied Physics, ETSI Minas, Universidad Politécnica de Madrid, C/Ríos Rosas 21, 28003 Madrid, SpainWe present an optical sensing methodology to estimate the fatigue damage state of structures made of carbon fiber reinforced polymer (CFRP), by measuring variations on the surface roughness. Variable amplitude loads (VAL), which represent realistic loads during aeronautical missions of fighter aircraft (FALSTAFF) have been applied to coupons until failure. Stiffness degradation and surface roughness variations have been measured during the life of the coupons obtaining a Pearson correlation of 0.75 between both variables. The data were compared with a previous study for Constant Amplitude Load (CAL) obtaining similar results. Conclusions suggest that the surface roughness measured in strategic zones is a useful technique for structural health monitoring of CFRP structures, and that it is independent of the type of load applied. Surface roughness can be measured in the field by optical techniques such as speckle, confocal perfilometers and interferometry, among others.http://www.mdpi.com/1424-8220/15/3/5710composite structuressurface roughnessfatigue damagevariable amplitude loadsoptical inspection
spellingShingle Pablo Zuluaga-Ramírez
Álvaro Arconada
Malte Frövel
Tomás Belenguer
Félix Salazar
Optical Sensing of the Fatigue Damage State of CFRP under Realistic Aeronautical Load Sequences
Sensors
composite structures
surface roughness
fatigue damage
variable amplitude loads
optical inspection
title Optical Sensing of the Fatigue Damage State of CFRP under Realistic Aeronautical Load Sequences
title_full Optical Sensing of the Fatigue Damage State of CFRP under Realistic Aeronautical Load Sequences
title_fullStr Optical Sensing of the Fatigue Damage State of CFRP under Realistic Aeronautical Load Sequences
title_full_unstemmed Optical Sensing of the Fatigue Damage State of CFRP under Realistic Aeronautical Load Sequences
title_short Optical Sensing of the Fatigue Damage State of CFRP under Realistic Aeronautical Load Sequences
title_sort optical sensing of the fatigue damage state of cfrp under realistic aeronautical load sequences
topic composite structures
surface roughness
fatigue damage
variable amplitude loads
optical inspection
url http://www.mdpi.com/1424-8220/15/3/5710
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