4.6 Article

Ultraviolet 3D digital image correlation applied for deformation measurement in thermal testing with infrared quartz lamps

Journal

CHINESE JOURNAL OF AERONAUTICS
Volume 33, Issue 3, Pages 1085-1092

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.cja.2019.03.038

Keywords

Deformation; DIC; Front-surface; Quartz lamp heating; Ultraviolet 3D digital image correlation

Funding

  1. National Natural Science Foundation of China [11602011, 11872009, 11632010]
  2. National S AMP
  3. T Major Project of China [ZX069]
  4. Aeronautical Science Foundation of China [2016ZD51034]
  5. Postdoctoral Science Foundation of China [2017M610029]

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In thermal-structural testing of hypersonic materials and structures, deformation measurement on the front surface of an object directly heated by quartz lamps is highly necessary and very challenging. This work describes a novel front-surface high-temperature deformation measurement technique, which adopts ultraviolet 3D digital image correlation (UV 3D-DIC) to observe and measure the high-temperature deformation fields on front surfaces directly heated by quartz lamps. Compared with existing blue light DIC techniques, the established UV 3D-DIC, which combines UV CCD camera, active UV illumination and bandpass filter imaging, can effectively suppress the strong disturbing light emitted by the quartz lamps and the heated sample itself during heating process. Two experiments were carried out to verify the robustness and accuracy of the developed technique: (1) direct observation of front surfaces of a hypersonic thermal structure sample heated from room temperature to 1050 degrees C, and (2) front-surface thermal stain and coefficient of thermal expansion (CTE) measurement of an Inconel 718 sample up to 800 degrees C. The well matched strain and CTE results with literature data show that UV 3D-DIC system is an effective technique for front-surface deformation measurement and has great potential in characterizing deformation response of hypersonic materials and structures subjected to transient aerodynamic heating. (C) 2019 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).

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