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Transport Phenomena.pdf

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172 Chapter 5 Velocity Distributions in Turbulent Flow<br />

Fig. 5.6-3. Streamline pattern in a circular jet in<br />

turbulent flow [H. Schlichting, Boundary-Layer Theory,<br />

McGraw-Hill, New York, 7th edition (1979),<br />

Fig. 24.10].<br />

eddy viscosity method seems to be somewhat better in the neighborhood of the maximum,<br />

whereas the mixing length results are better in the outer part of the jet.<br />

Once the velocity profiles are known, the streamlines can be obtained. From the streamlines,<br />

shown in Fig. 5.6-3, it can be seen how the jet draws in fluid from the surrounding mass<br />

of fluid. Hence the mass of fluid carried by the jet increases with the distance from the source.<br />

This mass rate of flow is<br />

w = pv z r dr de = 8TTP*/°Z (5.6-25)<br />

This result corresponds to an entry in Table 5.1-1.<br />

The two-dimensional jet issuing from a thin slot may be analyzed similarity. In that problem,<br />

however, the turbulent viscosity is a function of position.<br />

QUESTIONS FOR DISCUSSION<br />

1. Compare and contrast the procedures for solving laminar flow problems and turbulent flow<br />

problems.<br />

2. Why must Eq. 5.1-4 not be used for evaluating the velocity gradient at the solid boundary<br />

3. What does the logarithmic profile of Eq. 5.3-4 give for the fluid velocity at the wall Why does<br />

this not create a problem in Example 5.5-1 when the logarithmic profile is integrated over the<br />

cross section of the tube<br />

4. Discuss the physical interpretation of each term in Eq. 5.2-12.<br />

5. Why is the absolute value sign used in Eq. 5.4-4 How is it eliminated in Eq. 5.5-5<br />

6. In Example 5.6-1, how do we know that the momentum flow through any plane of constant z<br />

is a constant Can you imagine a modification of the jet problem in which that would not be<br />

the case<br />

7. Go through some of the volumes oi Ann. Revs. Fluid Mech. and summarize the topics in turbulent<br />

flow that are found there.<br />

8. In Eq. 5.3-1 why do we investigate the functional dependence of the velocity gradient rather<br />

than the velocity itself<br />

9. Why is turbulence such a difficult topic<br />

PROBLEMS<br />

5A.1 Pressure drop needed for laminar-turbulent transition. A fluid with viscosity 18.3 cp and<br />

density 1.32 g/cm 3 is flowing in a long horizontal tube of radius 1.05 in. (2.67 cm). For what<br />

pressure gradient will the flow become turbulent<br />

Answer: 42 psi/mi (1.8 X 10 5 Pa/km)

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