fluid_mechanics

claudia.marcela.becerra.rativa
from claudia.marcela.becerra.rativa More from this publisher
19.09.2019 Views

348 Chapter 7 ■ Dimensional Analysis, Similitude, and Modeling V7.3 Reynolds number No separation Re ≈ 0.2 Laminar boundary layer, wide turbulent wake Re ≈ 20,000 V7.4 Froude number The magnitude of the weight of the particle, F G , is F G gm, so the ratio of the inertia to the gravitational force is Thus, the force ratio F IF is proportional to V 2 G g/, and the square root of this ratio, V1g/, is called the Froude number. We see that a physical interpretation of the Froude number is that it is a measure of, or an index of, the relative importance of inertial forces acting on fluid particles to the weight of the particle. Note that the Froude number is not really equal to this force ratio, but is simply some type of average measure of the influence of these two forces. In a problem in which gravity 1or weight2 is not important, the Froude number would not appear as an important pi term. A similar interpretation in terms of indices of force ratios can be given to the other dimensionless groups, as indicated in Table 7.1, and a further discussion of the basis for this type of interpretation is given in the last section in this chapter. Some additional details about these important dimensionless groups are given below, and the types of application or problem in which they arise are briefly noted in the last column of Table 7.1. Reynolds Number. The Reynolds number is undoubtedly the most famous dimensionless parameter in fluid mechanics. It is named in honor of Osborne Reynolds 11842–19122, a British engineer who first demonstrated that this combination of variables could be used as a criterion to distinguish between laminar and turbulent flow. In most fluid flow problems there will be a characteristic length, /, and a velocity, V, as well as the fluid properties of density, r, and viscosity, m, which are relevant variables in the problem. Thus, with these variables the Reynolds number arises naturally from the dimensional analysis. The Reynolds number is a measure of the ratio of the inertia force on an element of fluid to the viscous force on an element. When these two types of forces are important in a given problem, the Reynolds number will play an important role. However, if the Reynolds number is very small 1Re 12, this is an indication that the viscous forces are dominant in the problem, and it may be possible to neglect the inertial effects; that is, the density of the fluid will not be an important variable. Flows at very small Reynolds numbers are commonly referred to as “creeping flows” as discussed in Section 6.10. Conversely, for large Reynolds number flows, viscous effects are small relative to inertial effects and for these cases it may be possible to neglect the effect of viscosity and consider the problem as one involving a “nonviscous” fluid. This type of problem is considered in detail in Sections 6.4 through 6.7. An example of the importance of the Reynolds number in determining the flow physics is shown in the figure in the margin for flow past a circular cylinder at two different Re values. This flow is discussed further in Chapter 9. Froude Number. The Froude number F I V 2 F G g/ V * dV * s s ds* Re rV/ m Fr V 1g/ is distinguished from the other dimensionless groups in Table 7.1 in that it contains the acceleration of gravity, g. The acceleration of gravity becomes an important variable in a fluid dynamics problem in which the fluid weight is an important force. As discussed, the Froude number is a measure of the ratio of the inertia force on an element of fluid to the weight of the element. It will generally be important in problems involving flows with free surfaces since gravity principally affects this type of flow. Typical problems would include the study of the flow of water around ships 1with the resulting wave action2 or flow through rivers or open conduits. The Froude number is named in honor of William Froude 11810–18792, a British civil engineer, mathematician, and naval architect who pioneered the use of towing tanks for the study of ship design. It is to be noted that the Froude number is also commonly defined as the square of the Froude number listed in Table 7.1.

7.6 Common Dimensionless Groups in Fluid Mechanics 349 The Mach number is a commonly used dimensionless parameter in compressible flow problems. V7.5 Strouhal number Euler Number. can be interpreted as a measure of the ratio of pressure forces to inertial forces, where p is some characteristic pressure in the flow field. Very often the Euler number is written in terms of a pressure difference, so that Also, this combination expressed as ¢p 1 2 ¢p, Eu ¢prV 2 . 2 rV is called the pressure coefficient. Some form of the Euler number would normally be used in problems in which pressure or the pressure difference between two points is an important variable. The Euler number is named in honor of Leonhard Euler 11707–17832, a famous Swiss mathematician who pioneered work on the relationship between pressure and flow. For problems in which cavitation is of concern, the dimensionless group 1 p r p v 2 1 2 2 rV is commonly used, where p v is the vapor pressure and p r is some reference pressure. Although this dimensionless group has the same form as the Euler number, it is generally referred to as the cavitation number. Cauchy Number and Mach Number. and the Mach number The Cauchy number are important dimensionless groups in problems in which fluid compressibility is a significant factor. Since the speed of sound, c, in a fluid is equal to c 1E v r 1see Section 1.7.32, it follows that r Ma V A E v and the square of the Mach number is equal to the Cauchy number. Thus, either number 1but not both2 may be used in problems in which fluid compressibility is important. Both numbers can be interpreted as representing an index of the ratio of inertial forces to compressibility forces. When the Mach number is relatively small 1say, less than 0.32, the inertial forces induced by the fluid motion are not sufficiently large to cause a significant change in the fluid density, and in this case the compressibility of the fluid can be neglected. The Mach number is the more commonly used parameter in compressible flow problems, particularly in the fields of gas dynamics and aerodynamics. The Cauchy number is named in honor of Augustin Louis de Cauchy 11789–18572, a French engineer, mathematician, and hydrodynamicist. The Mach number is named in honor of Ernst Mach 11838–19162, an Austrian physicist and philosopher. Strouhal Number. The Euler number Eu p rV 2 Ca rV 2 Ma V c Ma 2 rV 2 Ca E v The Strouhal number St v/ V is a dimensionless parameter that is likely to be important in unsteady, oscillating flow problems in which the frequency of the oscillation is v. It represents a measure of the ratio of inertial forces due to the unsteadiness of the flow 1local acceleration2 to the inertial forces due to changes in velocity from point to point in the flow field 1convective acceleration2. This type of unsteady flow may develop when a fluid flows past a solid body 1such as a wire or cable2 placed in the moving stream. For example, in a certain Reynolds number range, a periodic flow will develop downstream from a cylinder placed in a moving fluid due to a regular pattern of vortices that are shed from the body. 1See the photograph at the beginning of this chapter and Fig. 9.21.2 This system of vortices, called a Kármán vortex trail [named after Theodor von Kármán 11881–19632, a famous fluid E v

7.6 Common Dimensionless Groups in Fluid Mechanics 349<br />

The Mach number<br />

is a commonly used<br />

dimensionless parameter<br />

in compressible<br />

flow<br />

problems.<br />

V7.5 Strouhal<br />

number<br />

Euler Number.<br />

can be interpreted as a measure of the ratio of pressure forces to inertial forces, where p is some<br />

characteristic pressure in the flow field. Very often the Euler number is written in terms of a pressure<br />

difference, so that Also, this combination expressed as ¢p 1 2<br />

¢p, Eu ¢prV 2 .<br />

2 rV is called<br />

the pressure coefficient. Some form of the Euler number would normally be used in problems in<br />

which pressure or the pressure difference between two points is an important variable. The Euler<br />

number is named in honor of Leonhard Euler 11707–17832, a famous Swiss mathematician who<br />

pioneered work on the relationship between pressure and flow. For problems in which cavitation<br />

is of concern, the dimensionless group 1 p r p v 2 1 2<br />

2 rV is commonly used, where p v is the vapor<br />

pressure and p r is some reference pressure. Although this dimensionless group has the same form<br />

as the Euler number, it is generally referred to as the cavitation number.<br />

Cauchy Number and Mach Number.<br />

and the Mach number<br />

The Cauchy number<br />

are important dimensionless groups in problems in which <strong>fluid</strong> compressibility is a significant factor.<br />

Since the speed of sound, c, in a <strong>fluid</strong> is equal to c 1E v r 1see Section 1.7.32, it follows<br />

that<br />

r<br />

Ma V A E v<br />

and the square of the Mach number<br />

is equal to the Cauchy number. Thus, either number 1but not both2 may be used in problems in<br />

which <strong>fluid</strong> compressibility is important. Both numbers can be interpreted as representing an index<br />

of the ratio of inertial forces to compressibility forces. When the Mach number is relatively<br />

small 1say, less than 0.32, the inertial forces induced by the <strong>fluid</strong> motion are not sufficiently large<br />

to cause a significant change in the <strong>fluid</strong> density, and in this case the compressibility of the <strong>fluid</strong><br />

can be neglected. The Mach number is the more commonly used parameter in compressible flow<br />

problems, particularly in the fields of gas dynamics and aerodynamics. The Cauchy number is<br />

named in honor of Augustin Louis de Cauchy 11789–18572, a French engineer, mathematician, and<br />

hydrodynamicist. The Mach number is named in honor of Ernst Mach 11838–19162, an Austrian<br />

physicist and philosopher.<br />

Strouhal Number.<br />

The Euler number<br />

Eu <br />

p<br />

rV 2<br />

Ca rV 2<br />

Ma V c<br />

Ma 2 rV 2<br />

Ca<br />

E v<br />

The Strouhal number<br />

St v/<br />

V<br />

is a dimensionless parameter that is likely to be important in unsteady, oscillating flow problems<br />

in which the frequency of the oscillation is v. It represents a measure of the ratio of inertial forces<br />

due to the unsteadiness of the flow 1local acceleration2 to the inertial forces due to changes in velocity<br />

from point to point in the flow field 1convective acceleration2. This type of unsteady flow<br />

may develop when a <strong>fluid</strong> flows past a solid body 1such as a wire or cable2 placed in the moving<br />

stream. For example, in a certain Reynolds number range, a periodic flow will develop downstream<br />

from a cylinder placed in a moving <strong>fluid</strong> due to a regular pattern of vortices that are shed from the<br />

body. 1See the photograph at the beginning of this chapter and Fig. 9.21.2 This system of vortices,<br />

called a Kármán vortex trail [named after Theodor von Kármán 11881–19632, a famous <strong>fluid</strong><br />

E v

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!