Natural Convection Systems

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C H A P T E R 6 Natural Convection Systems 6.1 Physical Mechanism Of Natural Convection Many familiar heat transfer applications involve natural convection as the primary mechanism of heat transfer. Some examples are cooling of electronic equipment such as power transistors, TVs, and VCRs; heat transfer from electric baseboard heaters or steam radiators; heat transfer from the refrigeration coils and power transmission lines; and heat transfer from the bodies of animals and human beings. Natural convection in gases is usually accompanied by radiation of comparable magnitude except for low-emissivity surfaces. We know that a hot boiled egg (or a hot baked potato) on a plate eventually cools to the surrounding air temperature (Fig. 6 1). The egg is cooled by transferring heat by convection to the air and by radiation to the surrounding surfaces. Disregarding heat transfer by radiation, the physical mechanism of cooling a hot egg (or any hot object) in a cooler environment can be explained as follows: As soon as the hot egg is exposed to cooler air, the temperature of the outer surface of the egg shell will drop somewhat, and the temperature of the air adjacent to the shell will rise as a result of heat conduction from the shell to the air. Consequently, the egg will soon be surrounded by a thin layer of warmer air, and heat will then be transferred from this warmer layer to the outer layers of air. The cooling process in this case would be rather slow since the egg would always be blanketed by warm air, and it would have no direct contact with the cooler air farther away. We may not notice any air motion in the vicinity of the egg, but careful measurements indicate otherwise. Figure 6 1 The cooling of a boiled egg in a cooler environment by natural convection. Most heat transfer correlations in natural convection are based on experimental measurements. The lines of constant temperature for a natural convection on a hot vertical flat plate are shown in the Figure 6-2. The smooth and parallel lines in (a) indicate that the flow is laminar, whereas the eddies and irregularities in (b)

indicate that the flow is turbulent. Note that the lines are closest near the surface, indicating a higher temperature gradient. figure 6-2: a. Free convection laminar flow over isothermal hote plate, b. Free convection turbulent flow over isothermal hote plate. Natural Convection Over Surfaces Natural convection heat transfer on a surface depends on the geometry of the surface as well as its orientation. It also depends on the variation of temperature on the surface and the thermophysical properties of the fluid involved. The velocity and temperature profiles for natural convection over a vertical hot plate are shown in the Figure 6-3. Note that as in forced convection, the thickness of the boundary layer increases in the flow direction. Unlike forced convection, however, the fluid velocity is zero at the outer edge of the velocity boundary layer as well as at the surface of the plate. This is expected since the fluid beyond the boundary layer is motionless. Thus, the fluid velocity increases with distance from the surface, reaches a maximum, and gradually decreases to zero at a distance sufficiently far from the surface.

Figure 6-3: The velocity and temperature profiles for natural convection over a vertical hot plate. With the exception of some simple cases, heat transfer relations in natural convection are based on experimental studies. The simple empirical correlations for the average Nusselt number Nu in natural convection are of the form, Nu f = C GG f PG f m 6.1 Where C and m is the constants obtained from table 6-1. The product of the Grashof and Prandtl numbers is called the Rayleigh number: RR = GG PG GG = gβ( T )L c 3 v 2 Where: GG : Grashof number is the dimensionless used in the free convection. g : gravitational acceleration, =9.81 m/s 2 g = 1 T f, T f in kelvin. The turbulent case GG f PG f > 10 9

Characteristic Dimensions A s P

TABLE 6 1 Constants for use with Euation (6.1) for isothermal surfaces. Constant Heat Flux Surfaces GG x = GG x Nu x = gβq wx 4 6.2 kv 2 Where q w = q A s A s : Surface area, m 2. GG x PG > 2 10 13 turbulent flow The local heat-transfer coefficients were correlated by the following relation for the laminar range: 1 Nu xf = hx = 0.6 GG 5 k x PG f f 10 5 < GG x PG f < 10 11 laminar flow 6.3

Thus, for the laminar region, using Equation (6.3) to evaluate h x, h = 5 4 h x=l For the turbulent region, the local heat-transfer coefficients are correlated with 1 Nu xf = hx = 0.17 GG 4 k x PG f f 2 10 13 < GG x PG f < 10 16 turbulent 6.4 Thus, for the turbulent region, using Equation (6.4) to evaluate h x, h = h x=l All properties in Equations (6.3) and (6.4) are evaluated at the local film temperature. T f = +T 2 When the average Nusselt number and thus the average convection coefficient is known, the rate of heat transfer by natural convection from a solid surface at a uniform temperature to the surrounding fluid is expressed by Newton s law of cooling as q = ha( T )

Example 6.1: From Equation (6.2), with x=3.5 m, Use Equation (6.4), h = h x=l = 5.36 for turbulent flow with constant heat flux.

Example 6.2:

From Table 6-1, Example 6.3: RR = GGGG = gg(t 3 w T )L c PP v 2 From Table 6-1, Example 6.4:

From Table 6-1, Example 6.5: Table 6-1