Author Affiliations
1AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China2Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation, Beijing 100095, China3Key Laboratory of Aeronautical Materials Testing and Evaluation, Aero Engine Corporation of China, Beijing 100095, China4Aviation Key Laboratory of Science and Technology on Materials Testing and Evaluation, Beijing 100095, China5School of Materials Science and Engineering, Beihang University, Beijing 100191, Chinashow less
Fig. 1. 3D cylindrical model
Fig. 2. 2D model simplified from 3D cylindrical model
Fig. 3. Arrangement of defects in the specimen
Fig. 4. Simulation result of temperature difference ΔT(t) in different testing ambient temperature
Fig. 5. Simulation result of temperature contrast C(t) in different testing ambient temperature
Fig. 6. Positions of defect point and reference non-defect point in thermal image
Fig. 7. Experiment result of temperature difference ΔT(t) in different testing ambient temperature
Fig. 8. Experiment result of temperature contrast C(t) in different testing ambient temperature
Fig. 9. 2D model of uneven sunshine
Fig. 10. Simulation result of temperature difference ΔT(t) in uneven sunshine and in homogeneous temperature
Fig. 11. Simulation result of temperature contrast C(t) in uneven sunshine and in homogeneous temperature
Fig. 12. Thermal image t =1.102 s of the specimen in uneven sunshine before experiment
Fig. 13. Experiment result of temperature difference ΔT(t) in uneven sunshine and in homogeneous temperature
Fig. 14. Experiment result of temperature contrast C(t) in uneven sunshine and in homogeneous temperature
Fig. 15. Simulation result of temperature difference ΔT(t) in different wind velocity
Fig. 16. Simulation result of temperature contrast C(t) in different wind velocity
Fig. 17. Experiment result of temperature difference ΔT(t) in different wind velocity
Fig. 18. Experiment result of temperature contrast C(t) in different wind velocity
Specimen thickness
L/m
| Defect thickness
d/m
| Defect depth
l/m
| Specimen radius
R/m
| Defect radius
rd/m
| Heating pulse duration
t/s
| Heating flux density
q/W·m−2 | 0.0025 | 0.00005 | 0.0005 | 0.020 | 0.0075 | 0.002 | 0.84×107 |
|
Table 1. Main parameter in the model
Material | Density
ρ/kg·m−3 | Specific heat
cp/kJ·kg−1·K−1 | Thermal conductivity
λ/W·m−1·K−1 | GFRP[11] | 1900 | 1.2 | 0.3 | Air(20℃)[12] | 1.205 | 1.005 | 0.0259 | Air(30℃)[12] | 1.165 | 1.005 | 0.0267 |
|
Table 2. Thermal properties of materials