width = W
Height = H
Surface temp = T1
Maintained Room temperature = T2
Radiator surface emissivity = e
Part 1
energy is lost from radiation
Qrad = Ae (T14 - T24 )
Qrad = e x H x W x (T14 - T24 )
Part 2
Calculate the Reynolds number
Re = Length x velocity x density / viscosity
Fluid properties are constant at particular temperature
Prandtl number
Pr = specific heat capacity x viscosity / thermal conductivity
If Re < 2100
Flow is laminar
Heat transfer coefficient is calculated from seder tate equation
h = 0.027 (Re^0.8) (Pr^0.33) (/s)^(0.14)
If Re > 4000
Flow is turbulent
Heat transfer coefficient is calculated from dittus boelter equation
h = 0.023 (Re^0.8) (Pr^n)
For heating n = 0.4
For cooling n = 0.3
energy is lost from surface by convection
Qconv = hA (T1 - T2)
Part 3
proportion of total energy lost by radiation
= Qrad x 100 / (Qrad + Q conv)
Get Answers For Free
Most questions answered within 1 hours.