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104
CHAPTERS
1949 Guide ;
Table 2. ' ''
Appbohmate Unit Conductances fob Thebbal Convection .fob . Sevebal Flow Systems*
Expressed in Convenient Empirical Form
CASS;
. System
' Unit Conductance Equation* ...
Forced Convection
1-
Longitudinal flow In cylinders, turbulent region. Fluid being heated*.
- 0.0225 For (-^-) > 3000
2.
For longitudinal air flow in cylinders
1 he - 0.0036 <?*/** .
reduces to*.'
For > 3000
fto - 0.00486 (I + 0.010 AA
3. For longitudinal water flow in cylinders case 1
reduces to*.
For (-if-) > 3000
a -
4.
(A)Air flow normal to a single right circular
cylinder.
He - 0.45
+ 0.178
(A)"-"
5. Air flow over staggered pipe banka.
ho.- 0.081 (A )*'" C
Fundamentals of Heat Transfer
105
The heat transmission by free or natural convection for objects sur rounded by air can be conveniently expressed as in Equation 2a:
/i W i V" . __
,
where
qa = heat transmission by convection, Btu per (square foot) (hour).
q __ a constant depending upon the shape of the surface. D = diameter of pipe or circular duct or height of vertical wall, inches.
(Effect of diameter or height becomes constant at 24 in.) f> -- average of wall surface and surrounding air temperature, Fahrenheit
degrees absolute. .. t _ it -- temperature excess between wall surface and surrounding air, Fahren
heit degrees,
-
For horizontal cylinders, the value of C = 1.016 has been well estab lished by various investigations. For vertical plates, the value of C = 1.394 has been fairly well established. Suggested values2 of C for hori zontal plates warmer than the surrounding air are 1.79 when facing upward
and 0.89 when facing downward: Problems in either forced convection or natural convection may be solved
by the simple first-power equation if the convection coefficient is expressed
as a unit conductance:
6. Air flow over single spheres. 7. Air flow over plane surfaces. 8., Air flow normal, to finned cylinders.
* - 0-040 AA
0 <t < 250 F
h - 1 + 0.22 K. For V < 16 fps or Ac 0.53 K,-* 16 fps < F. < 100 fps
(-rr^-
0 <1 < 250 F
'
Free Convections
V'-. '
Single horizontal right circular cylinder in air. *-<>* (^-r
;, :;
10. Vertical surfaces in air.
*0 - 0.3
11. Top surface of horizontal plates to air. ho - 0.4
12.
Bottom surface of horizontal plates to air. ho = 0.2
* Heat Transmission, by W. H. McAdams.
k Fluid properties should be evaluated at the arithmetic mean fluid temperature, tf *=. (I*urfae +1 fluid)
divided by 2. '
*
;
> '' :
'
9 These expressions are applicable to longitudinal flow in other than right circular cylinders provided"the
hyrfrpnHn ro/finft fa o^iploytsf] ftp tha 'iifc dm*>n*^rin
For non-circular croea-eectiona D 4 fig
- d For low rates of-heat transfer by free convection the exponent decreases towards zero, and for. higher
. .. jrnatetbssininctreearmseesdtioawtearradnsg0e.33 The following equations employing an exponent equal to 0.25 are applicable
where
q0 a heat transmission by convection, Btu per hour.
A = surface area, square feet. lt -- = temperature difference between the surface and the fluid Fahrenheit
degrees.
*
h0 = unit conductance, from Table 2, Btu per (square foot) (hour) (Fahren
heit degree temperature difference.)
Thermal Radiation Equation The relation shown in Equation 3 is usually applicable to systems in
NOMENCLATURE AND DIMENSIONS FOR TABLE 2
Cp = fluid unit heat capacity at constant pressure, Btu per (pound) (Fahrenheit degree).
D = cylinder, diameter, feet. G = 3600 Vtp = fluid mass velocity, pounds per (hour) (square foot of flow
:cross-section). p = density, pounds per cubic foot. ha = unit conductance for thermal convection, Btu per (hour) (square foot)
(Farhrenheit degree). . k = unit thermal conductivity of the fluid, Btu per (hour) (square foot)
(Fahrenheit degree per one foot thickness). Rn = hydraulic radius of the flow cross-section = flow cross-section area.per
wetted perimeter/feet. s = fin spacing, feet. t = average fluid film temperature, Fahrenheit degree, h--fi = temperature difference surface to main fluid, Fahrenheit degree. Vt = fluid velocity, feet per second. P = fluid viscosity, pounds per (hour) (foot) = viscosity in centipoises X 2.42.