Thermal Mismatch Effect and High-Temperature Tensile Performance Simulation of Hybrid CMC and Superalloy Bolted Joint by Progressive Damage Analysis

<div>Axial stress contour maps of the composite plate for the joint with 1.2% clearance under various temperatures as the structure is subjected to failure. (a) 25°C. (b) 150°C. (c) 600°C. (d) 750°C.</div>

International Journal of Aerospace Engineering

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Figure 12

Figure 12: Thermal Mismatch Effect and High-Temperature Tensile Performance Simulation of Hybrid CMC and Superalloy Bolted Joint by Progressive Damage Analysis 

Figure 12 | Thermal Mismatch Effect and High-Temperature Tensile Performance Simulation of Hybrid CMC and Superalloy Bolted Joint by Progressive Damage Analysis 