fluid_mechanics
96 Chapter 3 ■ Elementary Fluid Dynamics—The Bernoulli Equation surroundings on the particle are indicated by the appropriate forces present, F 1 , F 2 , and so forth. For the present case, the important forces are assumed to be gravity and pressure. Other forces, such as viscous forces and surface tension effects, are assumed negligible. The acceleration of gravity, g, is assumed to be constant and acts vertically, in the negative z direction, at an angle u relative to the normal to the streamline. 3.2 F ma along a Streamline In a flowing fluid the pressure varies from one location to another. Consider the small fluid particle of size ds by dn in the plane of the figure and dy normal to the figure as shown in the free-body diagram of Fig. 3.3. Unit vectors along and normal to the streamline are denoted by ŝ and nˆ , respectively. For steady flow, the component of Newton’s second law along the streamline direction, s, can be written as a dF s dm a s dm V 0V 0s where g dF s represents the sum of the s components of all the forces acting on the particle, which has mass dm r dV, and V 0V0s is the acceleration in the s direction. Here, dV ds dn dy is the particle volume. Equation 3.2 is valid for both compressible and incompressible fluids. That is, the density need not be constant throughout the flow field. The gravity force 1weight2 on the particle can be written as dw g dV, where g rg is the specific weight of the fluid 1lbft 3 or Nm 3 2. Hence, the component of the weight force in the direction of the streamline is dw s dw sin u g dV sin u If the streamline is horizontal at the point of interest, then u 0, and there is no component of particle weight along the streamline to contribute to its acceleration in that direction. As is indicated in Chapter 2, the pressure is not constant throughout a stationary fluid 1§p 02 because of the fluid weight. Likewise, in a flowing fluid the pressure is usually not constant. In general, for steady flow, p p1s, n2. If the pressure at the center of the particle shown in Fig. 3.3 is denoted as p, then its average value on the two end faces that are perpendicular to the streamline are p dp s and p dp s . Since the particle is “small,” we can use a one-term Taylor series expansion for the pressure field 1as was done in Chapter 2 for the pressure forces in static fluids2 to obtain dp s 0p ds 0s 2 r dV V 0V 0s (3.2) g Particle thickness = δ y (p + δp n ) δs δy τ δs δy = 0 δn δs n δ δ n θ s θ (p + δp s ) δn δy (p – δp s ) δn δy δs δz θ Along streamline δ s τ δs δy = 0 (p – δp n ) δs δy θ δn δz Normal to streamline F I G U R E 3.3 Freebody diagram of a fluid particle for which the important forces are those due to pressure and gravity.
The net pressure force on a particle is determined by the pressure gradient. 3.2 F ma along a Streamline 97 Thus, if dF ps is the net pressure force on the particle in the streamline direction, it follows that dF ps 1p dp s 2 dn dy 1p dp s 2 dn dy 2 dp s dn dy 0p ds dn dy 0p 0s 0s dV Note that the actual level of the pressure, p, is not important. What produces a net pressure force is the fact that the pressure is not constant throughout the fluid. The nonzero pressure gradient, §p 0p0s ŝ 0p0n nˆ , is what provides a net pressure force on the particle. Viscous forces, represented by t ds dy, are zero, since the fluid is inviscid. Thus, the net force acting in the streamline direction on the particle shown in Fig. 3.3 is given by a dF s dw s dF ps ag sin u 0p 0s b dV By combining Eqs. 3.2 and 3.3, we obtain the following equation of motion along the streamline direction: g sin u 0p 0V rV (3.4) 0s 0s ra s We have divided out the common particle volume factor, dV, that appears in both the force and the acceleration portions of the equation. This is a representation of the fact that it is the fluid density 1mass per unit volume2, not the mass, per se, of the fluid particle that is important. The physical interpretation of Eq. 3.4 is that a change in fluid particle speed is accomplished by the appropriate combination of pressure gradient and particle weight along the streamline. For fluid static situations this balance between pressure and gravity forces is such that no change in particle speed is produced—the right-hand side of Eq. 3.4 is zero, and the particle remains stationary. In a flowing fluid the pressure and weight forces do not necessarily balance—the force unbalance provides the appropriate acceleration and, hence, particle motion. (3.3) E XAMPLE 3.1 Pressure Variation along a Streamline GIVEN Consider the inviscid, incompressible, steady flow along the horizontal streamline A–B in front of the sphere of radius a, as shown in Fig. E3.1a. From a more advanced theory of flow past a sphere, the fluid velocity along this streamline is FIND Determine the pressure variation along the streamline from point A far in front of the sphere 1x A and V A V 0 2 to point B on the sphere 1x B a and V B 02. as shown in Fig. E3.1b. V V 0 a1 a3 x 3b z 1 V o 0.75 V o V 0.5 V o V A = V ˆ O i V = Vi ˆ V B = 0 A B a x 0.25 V o (a) –3a –2a –1a 0 x (b) ∂p __ ∂x 0.610 ρV 2 0 /a p 2 0.5 ρV 0 –3a –2a –a 0 x (c) –3a –2a –a 0 x (d) F I G U R E E3.1
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96 Chapter 3 ■ Elementary Fluid Dynamics—The Bernoulli Equation<br />
surroundings on the particle are indicated by the appropriate forces present, F 1 , F 2 , and so forth.<br />
For the present case, the important forces are assumed to be gravity and pressure. Other forces,<br />
such as viscous forces and surface tension effects, are assumed negligible. The acceleration of gravity,<br />
g, is assumed to be constant and acts vertically, in the negative z direction, at an angle u relative<br />
to the normal to the streamline.<br />
3.2 F ma along a Streamline<br />
In a flowing <strong>fluid</strong><br />
the pressure varies<br />
from one location<br />
to another.<br />
Consider the small <strong>fluid</strong> particle of size ds by dn in the plane of the figure and dy normal to the<br />
figure as shown in the free-body diagram of Fig. 3.3. Unit vectors along and normal to the streamline<br />
are denoted by ŝ and nˆ , respectively. For steady flow, the component of Newton’s second law<br />
along the streamline direction, s, can be written as<br />
a dF s dm a s dm V 0V<br />
0s<br />
where g dF s represents the sum of the s components of all the forces acting on the particle, which<br />
has mass dm r dV, and V 0V0s is the acceleration in the s direction. Here, dV ds dn dy is<br />
the particle volume. Equation 3.2 is valid for both compressible and incompressible <strong>fluid</strong>s. That<br />
is, the density need not be constant throughout the flow field.<br />
The gravity force 1weight2 on the particle can be written as dw g dV, where g rg is<br />
the specific weight of the <strong>fluid</strong> 1lbft 3 or Nm 3 2. Hence, the component of the weight force in the<br />
direction of the streamline is<br />
dw s dw sin u g dV sin u<br />
If the streamline is horizontal at the point of interest, then u 0, and there is no component of<br />
particle weight along the streamline to contribute to its acceleration in that direction.<br />
As is indicated in Chapter 2, the pressure is not constant throughout a stationary <strong>fluid</strong> 1§p 02<br />
because of the <strong>fluid</strong> weight. Likewise, in a flowing <strong>fluid</strong> the pressure is usually not constant. In general,<br />
for steady flow, p p1s, n2. If the pressure at the center of the particle shown in Fig. 3.3 is<br />
denoted as p, then its average value on the two end faces that are perpendicular to the streamline are<br />
p dp s and p dp s . Since the particle is “small,” we can use a one-term Taylor series expansion<br />
for the pressure field 1as was done in Chapter 2 for the pressure forces in static <strong>fluid</strong>s2 to obtain<br />
dp s 0p ds<br />
0s 2<br />
r dV V<br />
0V<br />
0s<br />
(3.2)<br />
<br />
g<br />
Particle thickness = δ y<br />
(p + δp n ) δs δy<br />
τ δs δy<br />
= 0<br />
δn<br />
δs<br />
n<br />
δ <br />
δ <br />
n<br />
θ<br />
s<br />
θ<br />
(p + δp s ) δn δy<br />
(p – δp s ) δn δy<br />
δs<br />
δz<br />
θ<br />
Along streamline<br />
δ s<br />
τ δs δy<br />
= 0<br />
(p – δp n ) δs δy<br />
θ<br />
δn<br />
δz<br />
Normal to streamline<br />
F I G U R E 3.3 Freebody<br />
diagram of a <strong>fluid</strong> particle for<br />
which the important forces are those<br />
due to pressure and gravity.