Computational Fluid Dynamics Analysis of Impingement Heat Transfer in an Inline Array of Multiple Jets

Table 1

Boundary conditions used for computation.

Physical location/identity	Boundary type	Mathematical representation
Top plate/nozzle plate	Wall	u =  =  = 0; Ts = 300 K
Bottom surface/impingement plate	Wall	u =  =  = 0; q″ = 8333 W/m^2
Side/opening/outlet	Pressure outlet	P = Patm
Rear/side surface	Symmetry
Inlet/velocity inlet	Velocity inlet	As per value of Re at the nozzle
Nozzle walls	Wall	u =  =  = 0; T = 300 K