fluid_mechanics
188 Chapter 5 ■ Finite Control Volume Analysis Newton’s second law of motion leads to the conclusion that forces can result from or cause changes in a flowing fluid’s velocity magnitude and/or direction. Moment of force 1torque2 can result from or cause changes in a flowing fluid’s moment of velocity. These forces and torques can be associated with work and power transfer. The first law of thermodynamics is a statement of conservation of energy. The second law of thermodynamics identifies the loss of energy associated with every actual process. The mechanical energy equation based on these two laws can be used to analyze a large variety of steady, incompressible flows in terms of changes in pressure, elevation, speed, and of shaft work and loss. Good judgment is required in defining the finite region in space, the control volume, used in solving a problem. What exactly to leave out of and what to leave in the control volume are important considerations. The formulas resulting from applying the fundamental laws to the contents of the control volume are easy to interpret physically and are not difficult to derive and use. Because a finite region of space, a control volume, contains many fluid particles and even more molecules that make up each particle, the fluid properties and characteristics are often average values. In Chapter 6 an analysis of fluid flow based on what is happening to the contents of an infinitesimally small region of space or control volume through which numerous molecules simultaneously flow (what we might call a point in space) is considered. 5.1 Conservation of Mass—The Continuity Equation The amount of mass in a system is constant. 5.1.1 Derivation of the Continuity Equation A system is defined as a collection of unchanging contents, so the conservation of mass principle for a system is simply stated as or time rate of change of the system mass 0 DM sys where the system mass, M sys , is more generally expressed as Dt 0 (5.1) M sys sys r dV (5.2) and the integration is over the volume of the system. In words, Eq. 5.2 states that the system mass is equal to the sum of all the density-volume element products for the contents of the system. For a system and a fixed, nondeforming control volume that are coincident at an instant of time, as illustrated in Fig. 5.1, the Reynolds transport theorem 1Eq. 4.192 with B mass and b 1 allows us to state that D Dt sys r dV 0 0t cv r dV cs rV nˆ dA (5.3) System Control Volume (a) (b) (c) F I G U R E 5.1 System and control volume at three different instances of time. (a) System and control volume at time t Dt. (b) System and control volume at time t, coincident condition. (c) System and control volume at time t Dt.
V Control surface ^ n ^ Vn < 0 V ^ n ^ Vn > 0 or time rate of change of the mass of the coincident system In Eq. 5.3, we express the time rate of change of the system mass as the sum of two control volume quantities, the time rate of change of the mass of the contents of the control volume, and the net rate of mass flow through the control surface, 5.1 Conservation of Mass—The Continuity Equation 189 time rate of change net rate of flow of the mass of the of mass through contents of the coincident control volume the control surface 0 0t cv r dV cs rV nˆ dA When a flow is steady, all field properties 1i.e., properties at any specified point2 including density remain constant with time and the time rate of change of the mass of the contents of the control volume is zero. That is, 0 0t r dV0 cv The integrand, V nˆ dA, in the mass flowrate integral represents the product of the component of velocity, V, perpendicular to the small portion of control surface and the differential area, dA. Thus, V nˆ dA is the volume flowrate through dA and rV nˆ dA is the mass flowrate through dA. Furthermore, as shown in the sketch in the margin, the sign of the dot product V nˆ is “” for flow out of the control volume and “” for flow into the control volume since nˆ is considered positive when it points out of the control volume. When all of the differential quantities, rV nˆ dA, are summed over the entire control surface, as indicated by the integral cs rV nˆ dA the result is the net mass flowrate through the control surface, or The continuity equation is a statement that mass is conserved. cs rV nˆ dA a m # out a m # in where m # is the mass flowrate 1lbms, slugs or kgs2. If the integral in Eq. 5.4 is positive, the net flow is out of the control volume; if the integral is negative, the net flow is into the control volume. The control volume expression for conservation of mass, which is commonly called the continuity equation, for a fixed, nondeforming control volume is obtained by combining Eqs. 5.1, 5.2, and 5.3 to obtain 0 0t cv r dV cs rV nˆ dA 0 (5.4) (5.5) In words, Eq. 5.5 states that to conserve mass the time rate of change of the mass of the contents of the control volume plus the net rate of mass flow through the control surface must equal zero. Actually, the same result could have been obtained more directly by equating the rates of mass flow into and out of the control volume to the rates of accumulation and depletion of mass within the control volume 1see Section 3.6.22. It is reassuring, however, to see that the Reynolds transport theorem works for this simple-to-understand case. This confidence will serve us well as we develop control volume expressions for other important principles. An often-used expression for mass flowrate, m # , through a section of control surface having area A is m # rQ rAV (5.6)
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V<br />
Control<br />
surface<br />
^<br />
n<br />
^<br />
Vn < 0<br />
V<br />
^<br />
n<br />
^<br />
Vn > 0<br />
or<br />
time rate of change<br />
of the mass of the<br />
coincident system<br />
In Eq. 5.3, we express the time rate of change of the system mass as the sum of two control volume<br />
quantities, the time rate of change of the mass of the contents of the control volume,<br />
and the net rate of mass flow through the control surface,<br />
5.1 Conservation of Mass—The Continuity Equation 189<br />
<br />
time rate of change net rate of flow<br />
of the mass of the of mass through<br />
<br />
contents of the coincident<br />
control volume<br />
the control<br />
surface<br />
0<br />
0t cv<br />
r dV<br />
cs<br />
rV nˆ dA<br />
When a flow is steady, all field properties 1i.e., properties at any specified point2 including<br />
density remain constant with time and the time rate of change of the mass of the contents of the<br />
control volume is zero. That is,<br />
0<br />
0t r dV0<br />
cv<br />
The integrand, V nˆ dA, in the mass flowrate integral represents the product of the component<br />
of velocity, V, perpendicular to the small portion of control surface and the differential area,<br />
dA. Thus, V nˆ dA is the volume flowrate through dA and rV nˆ dA is the mass flowrate through<br />
dA. Furthermore, as shown in the sketch in the margin, the sign of the dot product V nˆ is “”<br />
for flow out of the control volume and “” for flow into the control volume since nˆ is considered<br />
positive when it points out of the control volume. When all of the differential quantities, rV nˆ dA,<br />
are summed over the entire control surface, as indicated by the integral<br />
cs<br />
rV nˆ dA<br />
the result is the net mass flowrate through the control surface, or<br />
The continuity<br />
equation is a statement<br />
that mass is<br />
conserved.<br />
cs<br />
rV nˆ dA a m # out a m # in<br />
where m # is the mass flowrate 1lbms, slugs or kgs2. If the integral in Eq. 5.4 is positive, the net flow<br />
is out of the control volume; if the integral is negative, the net flow is into the control volume.<br />
The control volume expression for conservation of mass, which is commonly called the continuity<br />
equation, for a fixed, nondeforming control volume is obtained by combining Eqs. 5.1, 5.2,<br />
and 5.3 to obtain<br />
0<br />
0t cv<br />
r dV cs<br />
rV nˆ dA 0<br />
(5.4)<br />
(5.5)<br />
In words, Eq. 5.5 states that to conserve mass the time rate of change of the mass of the contents<br />
of the control volume plus the net rate of mass flow through the control surface must equal zero.<br />
Actually, the same result could have been obtained more directly by equating the rates of mass flow<br />
into and out of the control volume to the rates of accumulation and depletion of mass within the<br />
control volume 1see Section 3.6.22. It is reassuring, however, to see that the Reynolds transport theorem<br />
works for this simple-to-understand case. This confidence will serve us well as we develop<br />
control volume expressions for other important principles.<br />
An often-used expression for mass flowrate, m # , through a section of control surface having<br />
area A is<br />
m # rQ rAV<br />
(5.6)