Yurim Park
- Embedded fiber Bragg grating sensor–based wing load monitoring system for composite aircraft. Dans: Structural Health Monitoring, v. 18, n. 4 (avril 2018). (2018):
- Application of silicon carbide fibers as a sensor for low-velocity impact detection and localization. Dans: Structural Health Monitoring, v. 18, n. 5-6 (septembre 2018). (2018):
- Design and Verification of Simultaneously Self-Sensing and Microwave-Absorbing Composite Structures based on Embedded SiC Fiber Network. Dans: Composite Structures, v. 261 (avril 2021). (2021):
- Behavior of Shear Thickening Fluid (STF) impregnated fabric composite rear wall under hypervelocity impact. Dans: Composite Structures, v. 204 (novembre 2018). (2018):
- Error outlier with weighted Median Absolute Deviation threshold algorithm and FBG sensor based impact localization on composite wing structure. Dans: Composite Structures, v. 180 (novembre 2017). (2017):
- Impact localization on composite structure using FBG sensors and novel impact localization technique based on error outliers. Dans: Composite Structures, v. 142 (mai 2016). (2016):
- Numerical simulation and empirical comparison of the high velocity impact of STF impregnated Kevlar fabric using friction effects. Dans: Composite Structures, v. 125 (juillet 2015). (2015):
- Impact localization on composite wing using 1D array FBG sensor and RMS/correlation based reference database algorithm. Dans: Composite Structures, v. 125 (juillet 2015). (2015):
- Hypervelocity impact on carbon/epoxy composites in low Earth orbit environment. Dans: Composite Structures, v. 96 (février 2013). (2013):
- Embedded silicon carbide fiber sensor network based low-velocity impact localization of composite structures. Dans: Smart Materials and Structures, v. 29, n. 5 (27 mars 2020). (2020):
- Strain sensing characteristics using piezoresistivity of semi-conductive silicon carbide fibers. Dans: Smart Materials and Structures, v. 28, n. 10 (29 août 2019). (2019):
- Low-velocity impact localization in a stiffened composite panel using a normalized cross-correlation method. Dans: Smart Materials and Structures, v. 24, n. 4 (avril 2015). (2015):
- Aircraft health and usage monitoring system for in-flight strain measurement of a wing structure. Dans: Smart Materials and Structures, v. 24, n. 10 (octobre 2015). (2015):