Modeling of Dynamic Behavior of Carbon Fiber-Reinforced Polymer (CFRP) Composite under X-ray Radiation
Abstract
:1. Introduction
2. Mechanism of Stress-Wave Induced by X-ray Pulse
2.1. X-ray Radiation and Energy Deposition
2.2. Stress Induced by Blow-Off Impulse (BOI) and Thermal Expansion
2.3. Elastic Constitutive Model
2.4. Plastic Constitutive Model
2.5. Modified Equation-of-State (EOS)
3. Finite Element Model (FEM)
3.1. In-House FEM Code Implementation
3.2. Geometry and Boundary Conditions
3.3. Material Properties
4. Results and Discussion
4.1. FEM Program Validation
4.2. Dynamic Response ofCarbon Fiber-Reinforced Polymer(CFRP) Composite under Various X-ray Radiations
5. Conclusions
- (1)
- The FE prediction of BOI momentum in an aluminum panel was at the same level as the experimental result, indicating the effectiveness of the FE model.
- (2)
- Compared to the aluminum panel, the CFRP panel effectively reduced the BOI and peak stress under the same radiation condition.
- (3)
- The FE results revealed that 1 keV X-ray resulted in surface vaporization, whereas no surface vaporization was seen when 3 keV X-ray was used, although front-surface spallation was seen in both cases. Furthermore, the magnitude of the stress wave under 1 keV X-ray was higher than that under 3 keV X-ray.
6. Patents
Acknowledgments
Author Contributions
Conflicts of Interest
References
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Elastic Parameters | Plastic Parameters | EOS Parameters | Failure Parameters | ||||
---|---|---|---|---|---|---|---|
E11 (GPa) | 9.7 | a11 | 0.669 | K′ (GPa) | 25.04 | σ11 (GPa) | 0.2457 |
E22 (GPa) | 72.9 | a22 | 0.025 | 1.098 | σ22 (GPa) | 0.6190 | |
E33 (GPa) | 22.89 | a33 | 1 | s | 1.049 | σ33 (GPa) | 0.1950 |
v12 | 0.0187 | a12 | 0 | γ | 1.667 | σ12 (GPa) | 0.0475 |
v13 | 0.218 | a13 | −0.471 | Estimated c0 (m/s) | 4003 | σ13 (GPa) | 0.0285 |
v23 | 0.77 | a23 | −0.128 | ρ0 (g/cm3) | 1.563 | σ23 (GPa) | 0.0393 |
G12 (GPa) | 0.873 | a44 | 0.061 | Estimated e0 (kJ/g) | 21.5 | ||
G13 (GPa) | 0.558 | a55 | 3.157 | ||||
G23 (GPa) | 48.35 | a66 | 2.128 |
Elastic Parameters | Plastic Parameters | EOS Parameters | Failure Parameters | ||||
---|---|---|---|---|---|---|---|
E (GPa) | 71.71 | k (GPa) | 0.5 | K (GPa) | 78.73 | σ (GPa) | 1.2 |
v | 0.33 | 2.18 | |||||
G (GPa) | 27.1 | s | 1.35 | ||||
γ | 1.667 | ||||||
c0 (m/s) | 5400 | ||||||
ρ0 (g/cm3) | 2.7 | ||||||
e0 (kJ/g) | 13.5 |
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Zhang, K.; Tang, W.; Fu, K. Modeling of Dynamic Behavior of Carbon Fiber-Reinforced Polymer (CFRP) Composite under X-ray Radiation. Materials 2018, 11, 143. https://doi.org/10.3390/ma11010143
Zhang K, Tang W, Fu K. Modeling of Dynamic Behavior of Carbon Fiber-Reinforced Polymer (CFRP) Composite under X-ray Radiation. Materials. 2018; 11(1):143. https://doi.org/10.3390/ma11010143
Chicago/Turabian StyleZhang, Kun, Wenhui Tang, and Kunkun Fu. 2018. "Modeling of Dynamic Behavior of Carbon Fiber-Reinforced Polymer (CFRP) Composite under X-ray Radiation" Materials 11, no. 1: 143. https://doi.org/10.3390/ma11010143