Transactions of Nanjing University of Aeronautics & Astronautics
Archive > Volume 35 Issue 2 > 2018,35(2):309-317. DOI:10.16356/j.1005-1120.2018.02.309 Prev Next

Non-Destructive Testing and Structural Health Monitoring in Aerospace 2018

Zemax-Based Optimum Structural Design of Probe of an Optical-Fiber Sensor

CHINA AERO-SCIENCES

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