【摘要】 为深化本科生对机翼结构在结构健康监测和应变测量的理解，使学生做到“知识-能力-素质”贯通，研制机翼悬臂梁结构应变测量的教学实验系统，引入光纤传感器、光纤光栅传感器测量方法及数字图像相关技术，开展全场应变场测量实验，并和传统的电测法进行对比，使学生了解和掌握先进的应变测量方法，同时对机翼悬臂梁结构进行有限元建模和求解，并将仿真结果和实验结果进行对比，使学生进一步理解先进应变测量方法的优势和应用前景，来提高学生分析问题、解决问题和独立研究的能力。实践表明：机翼结构应变测量实验与理论教学有机融合，有助于学生对综合分析、知识应用能力以及工程思维和素质的培养。更多还原

【Abstract】 In order to deepen the understanding of undergraduate students in structural health monitoring and strain measurement of wing structures, and to enable students to achieve the integration of “knowledge ability quality”, a teaching experimental system for strain measurement of wing cantilever beam structures is developed. Fiber optic sensors, fiber Bragg grating sensors measurement methods, and digital image related technologies are introduced to conduct full field strain field measurement experiments, and compared with traditional electrical measurement methods, so that students can understand and master advanced strain measurement methods. At the same time, finite element modeling and solving of wing cantilever beam structures are carried out, and simulation results are compared with experimental results to further understand the advantages and application prospects of advanced strain measurement methods. This improves students’ ability to analyze, solve problems, and conduct independent research. Practice has shown that the organic integration of wing structure strain measurement experiments and theoretical teaching helps students cultivate their comprehensive analysis, knowledge application abilities, engineering thinking and quality.更多还原