External_Flow_Plate
Procedure External_Flow_Plate(Fluid$, T_inf, T_s, P, V, L: tau, h, C_f, Nusselt, Re) calculates the average heat transfer coefficient and the coefficient of friction for external flow over a flat plate. The propeties are evaluated at the film temperature and the units of the inputs and outputs correspond to the settings in EES. (Note that the shear stress is returned in either Pa or psi units.)
Inputs
Fluid$ can be any fluid in the EES data base. The fluid can be an ideal gas, a real fluid, a brine, or an incompressible fluid in the Solid-Liquid_Props fluids library.
T_inf - the free stream fluid temperature in [C], [K], [F], or [R].
T_s - the surface temperature of the sphere in [C], [K], [F], or [R].
P - pressure can be in [Pa], [kPa], [bar], [MPa], [atm], or [psia]. (Note that for brines, this parameter provides the concentration in % instead of pressure.)
u_inf - free stream velocity of flow in [m/s] or [ft/min]
L - length of the plate in [m] or [ft]
Outputs
tau - average shear stress [Pa] or [psi]
h - average heat transfer coefficient in [W/m^2-K] or [Btu/hr-ft^2-R]
C_f - average coefficient of friction [-], defined as:
where
r is the density of the fluid
Nusselt - average Nusselt number [-], defined as:
where
k is the conductivity of the fluid
Re - Reynolds number [-], defined as:
where
m is the viscosity of the fluid
Notes
This procedure determines the property data of the specified fluid and calculatesthe Reynolds and Prandtl numbers. The Prandtl, Reynolds and Nusselt numbers are based on the film temperature, which is the average of the free stream and the surface temperatures. This procedure then passes the Reynolds and Prandtl numbers to the non-dimensional procedure External_Flow_Plate_ND. The non-dimensional procedure then returns the values for C_f and Nusselt and External_Flow_Plate calculates the average shear stress and the convection heat transfer coefficient.
Example
$unitSystem SI K Pa J
T_s=328 [K]
Fluid$='air'
T_inf=297 [K]
P=101300 [Pa]
u_inf=7 [m/s]
L=0.5 [m]
Call External_Flow_Plate(Fluid$, T_inf, T_s, P, u_inf, L: tau, h, C_f, Nusselt, Re)
{Solution: tau=0.08088 [Pa], h=14.15 [W/m^2-K], C_f=0.002923, Nusselt=266.3 [-], Re=206,382 [-]}