Laser & Optoelectronics Progress, Volume. 62, Issue 1, 0122002(2025)
Design of Strain and Temperature Field Endoscopic Detection System for Hot-End Components of Aircraft
Fig. 6. MTF curves and relative illuminance curves under different wavelengths. (a)(c) λ=440 nm; (b)(d) λ=530 nm
Fig. 7. Simulated image results at 20 ℃. (a) Test images; (b) λ=440 nm; (c) λ=530 nm
Fig. 8. MTF curves at different temperatures. (a) T′=50 ℃, λ=440 nm; (b) T′=50 ℃, λ=530 nm; (c) T′=150 ℃, λ=440 nm; (d) T′=150 ℃, λ=530 nm; (e) T′=250 ℃, λ=440 nm; (f) T′=250 ℃, λ=530 nm
|
|
|
|
|
Get Citation
Copy Citation Text
Hao Wang, Kun Du, Zhiming Xie, Jing Zhu, Huijie Huang. Design of Strain and Temperature Field Endoscopic Detection System for Hot-End Components of Aircraft[J]. Laser & Optoelectronics Progress, 2025, 62(1): 0122002
Category: Optical Design and Fabrication
Received: Apr. 11, 2024
Accepted: Apr. 29, 2024
Published Online: Jan. 6, 2025
The Author Email:
CSTR:32186.14.LOP241083