Document pm6wZNYJBOnDpeOgYMq1bnd97
68
CHAPTER 4
1954 Guide
Replacing v by its equal g/g<# (wherep is density in pounds weight per cubic foot) and rearranging, Equation 3 becomes
-- dV* + - dp + dz + -- [J du + p dv -- J dg + dW] = 0
2g p
g
(4)
In the case of flow through a pipe, no outside work is performed so that
dW. = 0. Furthermore,
J du + p dv = JT ds = J dg + JTds'
(5)
where
ds -- total change in entropy. ds' = change in entropy due to internal irreversibility from turbulence and
friction.
Fluid Flow
69
pipe diameter were the same throughout, the velocity, and consequently the velocity head, would be the same at both points, but the higher elevation at point 2 would still be responsible for a loss in pressure. The utility of the equation is evident, though it should be remembered that in it the effects of friction and turbulence are neglected, and that Fig. I
represents ideal conditions. It should also be noted that, care must be taken in determining the proper mean density. Accordingly, the Bernoulli
equation is applied most conveniently to incompressible fluids for which density is constant,
Fig. 1. Relation of Various Factors in Bernoulli Equation
Accordingly, Equation 4 may be written
- dV* + ^ + dz + - JTds' = 0*
2g p
9
(6)
In cases where there is no internal irreversibility, els' = 0, and Equation 6 may be integrated to give
5! + *+fc-5? + & + *
2g Pm
*9 Pra
(7)
where p ,, is the proper mean density. This is commonly called the Bernoulli equation, named after the Swiss
mathematician and physician who first propounded the theory. ^ is
known as the velocity head, - is the pressure head, and a is the elevation
head, all in feet of the fluid; the total head, At is the sum of the other three heads. Fig. 1 shows diagrammatically the relation of the various factors. The pressure at point 2 is lower than at point 1 because of the elevation of point 2 over point 1, and the velocity at point 2 is lower than at point 1 because of the larger pipe diameter at point 2. If the
* In the analysis of subsequent portions of this chapter the
Uiffluidflow
Aside from the dimensional consistency the factor, g(qc, is not in general signifies
Fig. 2. Relation of Kinematic Viscosity to Temperature of Air
Pressure Loss in Circular Pipes The pressure loss in circular pipes is customarily expressed by the
formula:
. _jflV* ' 2gd
where
hi = the loss in head of the fluid under conditions of flow, in feett l = the length of the pipe, in feet. V = the velocity, in feet per second. g = the acceleration due to gravity = 32.174 ft per (second) (second), d = the internal diameter of the pipe, in feet. / = a dimensionless friction coefficient.
(8)
The formula is generally known by the name of Darcy or Fanning, though it seems to have been originated by d'Aubisson de Voisins in 1834.
The factor/ is a function of the Reynolds number,
d Vp N R,
u
(9)