The eyeballs and the space between the manikin and the surrounding cube (shown in Fig. 5) are considered a computational domain. To study the flow field, the following assumptions are made: The airflow is incompressible and steady and around the manikin is in turbulent regime. The experiment of Clark and Toy [40] showed that the flow is laminar around a standing nude human for height shorter than 0.9m with (Tskin =306 K, Tair=293 K, and Grashof number = 2×109) but the regime becomes fully turbulent for a manikin taller than 1.5 m (Grashof number = 1010). The eyes are located on the head; therefore, assuming a turbulent flow around the manikin head is especially justified. It is assumed that the liquid flow in the eye anterior chamber is laminar because of the low velocity in the small anterior chamber.
The physical properties of air are constant and determined at the film temperature. Boussinesq approximation is adopted for the density variation since the temperature difference is sufficiently small with βΔT < < 1 [41]. The body force in these flows is only due to gravity.
Governing Equations
a) Temperature distribution inside the solid part of the eyeball is obtained by solving the following heat conduction equation [8]:
$$-\nabla . \left(k\nabla T\right)=A-B\left(T-{T}_{bl}\right)$$
1
where T is temperature, k is thermal conductivity, Tbl is blood temperature, A is the metabolic heat generation rate and B is the term associated with the blood perfusion rate. Only aqueous humor (AH) in the anterior chamber is considered liquid).
Governing equations of conservation of mass, momentum, and energy for laminar flow of aqueous humor (AH) are expressed as:
\(\nabla .\overrightarrow{v}=0\) | (2) |
---|
\(\rho (\overrightarrow{v}\bullet \nabla\)) | (3) |
\(\nabla \bullet \left(k\nabla T\right)-\rho C\left(\overrightarrow{v } \bullet \nabla T\right)=0\) | (4) |
where the Boussinesq approximation is used for density variation. Here, β is the fluid's volume expansion coefficient, C is heat capacity, and Tref =34 ˚C is a reference temperature.
Several turbulence models are investigated to predict the thermal plume due to natural convection. The RNG k-ε model with three different types of boundary conditions (scalable wall function, enhanced wall treatment, low Reynolds) and the SST k-ω model were used in the present study. Among these models, the RNG k-ε model with enhanced wall treatment is better matched to the experimental data for the heat transfer coefficient over the body and no inconsistent jump over the contours. Therefore, this model was used for further simulations.
All the testing steps are repeated for mixed convection, and the RNG k-ε model combined with the enhanced wall treatment option is selected for the rest of the simulations.
The details of the continuity, momentum, energy, and the RNG k-ε turbulence model equations are not shown here for brevity, and they can be found in (ANSYS manual).
Boundary Conditions
To investigate mixed convection heat transfer from the manikin, uniform air velocity with 6% turbulent intensity and 0.7 m length scale (approximately similar to the experimental conditions of De dear et al. [26]) is applied on the inlet boundary. Zero gradients for flow parameters are considered at the outlet boundary condition. Enhanced wall treatment boundary condition is used on wall surfaces such as the computational domain's manikin surface, bottom, upper and side walls. In addition, the symmetry and uniform velocity boundary conditions are also tested on the upper face and sides of the computational domain. Due to the use of sufficiently large computational domains, the effects of these different boundary conditions on the heat transfer from the manikin were found to be negligible. Therefore, the results can also resemble the outdoor conditions. Air with different velocities and temperatures as summarized in Table 3, are used on the inlet boundary of the computational domain. Manikin surface temperature is assumed to be 34 ˚C.
When the ambient air speed is less than 0.2 m/s, the heat transfer from the human skin is mainly treated as natural convection. The force convection has also been simulated for a velocity higher than this. The selected range of air velocity (0.2-5 m/s) covers indoor and outdoor environmental conditions.
Table 3
Environmental conditions for computations
Air velocity (m/s) | Environmental temperature (˚C) |
---|
0.0 | 0 | 20 |
0.3 | 0 | 20 |
1.0 | 0 | 20 |
5.0 | 0 | 20 |
To study natural convection conditions, a pressure inlet is applied on the side surfaces of the computational domain. Enhanced wall treatment is applied on the upper and lower surfaces of the domain.
Also, a zero gradient type boundary condition is considered an outlet boundary condition on the upper surface of the computational domain.
Numerical simulations are performed for two ambient air temperatures of 0, 20 ˚C. To consider heat flux between parts of the cornea and sclera that have contact with the inside of the body, the following equation is applied, respectively:
In this equation, the temperature of blood vessels Tbl, near the sclera is assumed to be constant, hs is the heat transfer coefficient between the inside of the body and the eye, B corresponds to the term associated with the blood perfusion rate, and A is the metabolic heat generation rate. Thermal properties and the quantities considered for Eq. (14) are summarized in Table 4 and Table 5.
Table 4
Thermal properties of the biological materials of eye layers
Material | Density ρ(hg m− 3) | Specific heat c(J kg− 1K− 1) | Thermal conductivity k(W m− 1K− 1) | Basal metabolism (W m− 3) | Blood perfusion power equivalent (W m-3 K-1) |
---|
Cornea | 1050a | 4178a | 0.58a | - | - |
Sclera | 1050a | 3800b | 0.58b | 22000b | 80000b |
Anterior chamber | 996a | 3997a | 0.58a | - | - |
Iris | 1050a | 3600b | 0.52b | 10000b | 35000b |
Lens | 1000a | 3000a | 0.4a | - | - |
Vitreous chamber | 1100a | 4178a | 0.603a | - | - |
a[38] |
b[42] |
Table 5
Physical parameters at the boundaries of the eye
Parameter | Description | Value |
---|
hs | Body heat transfer coefficient (W m− 2 K− 1) | 65a |
Tbl | Blood temperature (˚C) | 37 |
E | Evaporation rate (W m− 2) | 40a |
σ | Stefan-Boltzmann constant (W m− 2 K− 4) | 5.67×10− 8 |
ε | Emissivity of corneal surface | 0.975a |
a [38] |
No slip boundary condition on the anterior chamber surface, which is assumed to be rigid and impermeable, is imposed. Mechanical properties of eye layers are considered homogenous and isotropic.
To consider radiation heat transfer from the eye surface, the heat flux given as
is added to each element of the eye surface that is in contact with the environment. A UDF (User-defined function) was developed and incorporated into the ANSYS-FLUENT.
According to the previous studies of [21], the evaporation rate from a normal eye ranges from 40–100 W/m2. Here, the lowest value of E = 40 W/m2 is used to obtain the highest temperatures in the eye. The evaporation heat loss is included using the same procedure used for the radiation heat transfer.
The commercial fluid dynamic software package ANSYS-FLUENT is used for numerical simulation. An unstructured grid is developed for the environmental chamber around the manikin using the ANSYS (ICEM) software. To resolve the boundary layer around the eye, five layers of extruded triangular prisms are used with an initial size of 0.01 cm and a growth rate of 1.1 between the layers. Since the focus of the present study is the heat transfer from the eyes, most grid elements are placed around the head, particularly near the eyes, as shown in Fig. 6. The grids are fine near the manikin and become course far from the manikin.
Since the enhanced wall treatment is used as the turbulent wall boundary condition, the value of y+ should be less than 5 for the grid points adjacent to the manikin surface as a requirement for the used turbulence model. In these simulations, it is made sure that this condition is satisfied. For the case of natural convection with a body temperature of 34˚C and environmental temperature of 22 ˚C, the average value of y+ for the first grid points near the manikin body is equal to 0.62.
To generate a computational grid for the anterior eye chamber, a structured grid is used for the 2D geometry shown in Fig. 7. Then, by rotating this grid around the optical axis, the 3D structured grid is created.
The eye grid is integrated with the manikin grid using an unstructured grid in the cornea and sclera. To have a smooth transition between the structured grid inside the eye and the unstructured grid outside, rectangular elements on the outer surface of the structured grid are separated into two triangles by ANSYS (ICEM) software to be a base for the unstructured grid of cornea and sclera as illustrated in Fig. 8.
The grid independence study is performed for various grid sizes, and finally, the cases with about 5 and 6 million cells are selected for natural and mixed convection cases, respectively.