For the system described in Example 13.2, assume that the air inside the container is at 298 K, but the vessel wall is heated due to solar radiation. The temperature of air that flows out of the crack...

For the system described in Example 13.2, assume that the air inside the container is at 298 K, but the vessel wall is heated due to solar radiation. The temperature of air that flows out of the crack is 302 K. Using constant wall heat flux assumption as an approximation for the crack boundary conditions, estimate the temperature of the crack surface. Assume that both the momentum and thermal accommodation coefficients are equal to 0.85.