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Handbook of air conditioning and refrigeration / Shan K

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18.52 CHAPTER EIGHTEEN<br />

CFD Becomes More Popular<br />

HVAC&R engineers traditionally conducted scale-model physical experiments to study <strong>air</strong> motion<br />

<strong>and</strong> temperature distribution by maintaining similarity through a high Re number <strong>and</strong> an appropriate<br />

Ar corresponding to the adopted scale. CFD was first developed in Europe <strong>and</strong> Japan. In the<br />

late 1980s, ASHRAE organized a research project which thoroughly investigated many issues associated<br />

with CFD simulation. In the late 1990s, CFD became more popular in the HVAC&R industry<br />

for the determination <strong>of</strong> locations <strong>of</strong> supply outlets <strong>and</strong> return inlets, <strong>air</strong>flow patterns, <strong>air</strong> velocity<br />

<strong>and</strong> temperature distributions, <strong>and</strong> contaminant concentration <strong>and</strong> removal in an HVAC&R system.<br />

Baker et al. (1997) <strong>and</strong> Ladeinde <strong>and</strong> Neavon (1997) summarized the reasons for CFD’s popularity:<br />

● CFD has the ability to establish firm quantitative data regarding <strong>air</strong> motion <strong>and</strong> can predict fluid<br />

characteristics <strong>and</strong> pressure differentials to very low levels that are essentially impossible during<br />

experiments.<br />

● The cost <strong>of</strong> CFD is lower than that <strong>of</strong> scale-model experiments.<br />

● Earlier CFD codes were developed on supercomputers. Today computing s<strong>of</strong>tware is available for<br />

simulations to be performed on personal computers.<br />

● People are slowly getting over the fear <strong>of</strong> using CFD.<br />

Reynolds-Averaged Navier-Stokes Equations<br />

Numerical Methods<br />

The mathematical expressions describing the basic space-time relationship between mass, velocity,<br />

<strong>and</strong> temperature are expressed in partial differential equations called Navier-Stokes (NS) equations.<br />

These equations may be only directly applied to laminar flow fields. Baker et al. (1997) pointed out<br />

that CFD modeling based on NS equations requires a large number <strong>of</strong> assumptions <strong>and</strong> approximations.<br />

These approximations are closely related to the CFD computing results.<br />

For predicting turbulent flow, an approximation called Reynolds averaging (Ra) is used to<br />

convert this time-unsteady flow to a mean velocity presentation. A principal assumption for CFD is<br />

the turbulence closure model to govern the Reynolds-averaged Navier-Stokes partial differential<br />

equations. The selected CFD has been a two-equation turbulent kinetic energy (TKE) model. The<br />

TKE model assumes a fully turbulent flow existing everywhere for room <strong>air</strong>flow prediction. Actually,<br />

at normal <strong>air</strong> change rates per hour, fully turbulent flow occurs only in supply ducts, <strong>air</strong> jets,<br />

downstream <strong>of</strong> the edge <strong>of</strong> the obstacles. Elsewhere, the flow is more likely weakly turbulent <strong>and</strong><br />

actually time-unsteady. A quantitative measurement <strong>of</strong> the degree <strong>of</strong> turbulence <strong>of</strong> an <strong>air</strong>flow is the<br />

turbulence Reynolds number (Re t ) which is defined as the ratio <strong>of</strong> the turbulence eddy viscosity to<br />

the kinematic viscosity: Re t � v t /v. For laminar flow, Re t � 0, <strong>and</strong> for fully turbulent flow 50 �<br />

Re t � 10 3 .<br />

Because these Reynolds-averaged partial differential equations using the turbulence Reynold<br />

number Re t are highly nonlinear, they are not solvable by explicit, analytical methods. In these<br />

partial differential equations, the velocities u, v, w; <strong>and</strong> pressure p; temperature T; <strong>and</strong> some<br />

scalar � are dependent variables to be calculated. Space displacements x, y, z <strong>and</strong> time t are independent<br />

variables. Initial <strong>and</strong> boundary conditions must be specified. Numerical solution (approximate<br />

methods) such as via the finite element <strong>and</strong> finite volume methods is more popular in CFD<br />

simulation.<br />

Ladeinde <strong>and</strong> Neavon (1997) illustrated the finite element procedure during the calculation<br />

<strong>of</strong> <strong>air</strong>flow in a duct section. Figure 18.28a shows this duct section that contains an inlet <strong>and</strong> an<br />

outlet. The interior <strong>of</strong> the duct that constitutes the region <strong>of</strong> <strong>air</strong>flow (domain <strong>of</strong> the CFD model)

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