Optical Fiber Bragg Grating-Based Measurement of Fluid-Structure Interaction on a Cantilever Panel in High-Speed Flow

被引:0
作者
Pollock, Luke [1 ]
Kleine, Harald [1 ]
Neely, Andrew [1 ]
Wild, Graham [2 ]
机构
[1] Univ New South Wales UNSW Canberra, Sch Engn & Informat Technol, Canberra, ACT 2612, Australia
[2] Univ New South Wales UNSW Canberra, Sch Sci, Campbell, ACT 2612, Australia
关键词
Fiber gratings; Electric shock; Monitoring; Testing; Aerodynamics; Optical variables measurement; Biomedical monitoring; Bragg gratings; Thermal analysis; Supersonic flow; Structural health monitoring (SHM); integrated vehicle health monitoring (IVHM); fiber Bragg grating (FBG); fluid-structural interaction (FSI); fluid-thermal-structural interaction (FTSI); aeroelasticity; aerothermoelasticity; high-speed; supersonic; hypersonic; TEMPERATURE; SENSOR; COMPRESSION; STRAIN;
D O I
10.1109/ACCESS.2024.3430219
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Optical fiber Bragg grating (FBG) technology offers many advantages over conventional electrical sensors for the measurement of fluid-structure interaction (FSI). In this work, FBGs are used to measure the dynamic response of 3 mm, 2 mm, and 1 mm thick aluminum cantilever panels under the influence of Mach 2 reflected shock impingement in the UNSW Canberra supersonic blowdown facility. Results compared during start-up and steady-state with high-speed digital video schlieren and laser Doppler vibrometry indicate that FBGs can successfully capture the temporal and spectral characteristics of high-speed FSI. The torsional mode of the 1 mm plate is spectrally captured by the FBG with only a single sensor. Furthermore, it is shown that error in the FBG signal is comparable to that of a laser Doppler vibrometer. The greatest challenge remains the efficient decoupling of thermal effects.
引用
收藏
页码:101106 / 101120
页数:15
相关论文
共 47 条
[1]  
Anderson J. D., 2019, HYPERSONIC HIGH TEMP, P35, DOI DOI 10.2514/4.105142
[2]  
Axisa Francois., 2006, Modelling of Mechanical Systems: Fluid-Structure Interaction
[3]  
Aybar, 2006, SOBEL EDGE DETECTION, P26410
[4]  
Babinsky H., 2011, Shock Wave-Boundary-Layer Interactions, P19, DOI 10.1017/CBO9780511842757
[5]   DETERMINATION OF THE INDIVIDUAL STRAIN-OPTIC COEFFICIENTS IN SINGLE-MODE OPTICAL FIBERS [J].
BERTHOLDS, A ;
DANDLIKER, R .
JOURNAL OF LIGHTWAVE TECHNOLOGY, 1988, 6 (01) :17-20
[6]  
Bhattrai S., 2018, 22 AIAA INT SPAC PLA, P5265
[7]  
Bhattrai S., 2020, P 23 AIAA INT SPAC P, DOI [10.2514/6.2020-2449, DOI 10.2514/6.2020-2449]
[8]  
Brouwer K. R., 2021, AIAA SCITECH 2021, P0910
[9]   Simultaneous strain and temperature sensor based on the numerical reconstruction of polarization maintaining fiber Bragg gratings [J].
Caucheteur, C ;
Lhommé, F ;
Chah, K ;
Blondel, M ;
Mégret, P .
OPTICS AND LASERS IN ENGINEERING, 2006, 44 (05) :411-422
[10]  
Currao G. M., 2017, P 7 EUR C AER SPAC S, V12, P1