Mechanics

Nickolay Zosimovych, Manoj Kumar

Sharda University (India, UP)

PROBLEM STATEMENT FOR STATISTICAL MODELLING OF

NON-STATIONARY TURBULENT FLOW IN THE PIPES

 

Summary. In this paper studies the task of the statistical model unsteady turbulent flow through a pipe using the local quasistationary performance of turbulence.

Key words: flow, pipe, turbulence, experimental data, statistical model, pressure, characteristics of a flow, unsteady turbulent moving, pulsations, viscous fluid, a pressure gradient, component of velocity, energy equation.

Introduction. The flow in a long pipe on enough big distance from its ends is one of examples of shift turbulent flow [1]. Unlike a flow in an interface or as a stream without compressibility, the average characteristic of movement, the distribution of speed on radius, depends only from one spatial coordinate [2]. Models of turbulent flows in pipes are semiempirical, with use of the constants usually received by practical consideration [3, 4]. Mathematical models of unsteady flows become more and more complicating. In them there are no experimental data about influence unsteady flows on the constants entering into semiempirical dependences. Therefore it is necessary to use the assumption about quasi steady flow [5].

In the given work it is necessary to investigate the statistical model of unsteady turbulent flow in a pipe with use of local quasi steady characteristics of turbulence. The offered model allows to investigate more detailed the features of unsteady turbulent flow, and in particular, local kinematic characteristics of turbulence, energy dissipation, instant values of pressure of a friction about walls and so on. Calculations on statistical model give us the chance to compare with the data of experiments both integrated, and local characteristics of a flow that is rather interesting from the point of view of check of correctness of the most quasi stationary model.

Problem statement. Following the work [6], we will consider an unsteady turbulent moving of an incompressible viscous fluid in a round cylindrical pipe, in the assumption that the flow is not turbulent moving (there is an axial symmetry) and is statistically homogeneous along a pipe axis, that is average values of speed, and product of pulsations of speed do not depend on from coordinate  Using these assumptions and conditions of tightness of a wall of a pipe, from the equation of indissolubility [7] it is received that  Taking into account stated above assumptions, the system of the equations of a turbulence moving assumes the following air [6, 8]:

      

                            

 

 

 

 

 

 

(1)

Having excluded the second equation for a pressure gradient in a radial direction in system (1) and integrating on radius, we will receive

                                          (2)

where  value of pressure at the wall at  From dependence (2) follows that pressure changes on pipe radius. If we differentiating the equation (2) with the account that according to the accepted assumptions also do not depend from that is function only and as well as size   

If to analyze the first equation in system (1) it will be found out that according to assumptions all members, except the last, do not depend from  Hence, from should not depend on last member, i.e. the function only time.

Parts enter into the equation of turbulent energy (2) (in square brackets), pressure of viscous forces friction describing work. It is known that work of forces of viscous pressure in a turbulent stream is essential only in immediate proximity from a wall. Thus the basic contribution to work of viscous pressure brings part  [9]. Accordingly, the other parts in the brackets can be ignored.  After simplifications [7], the system equations reduce in two equations - Reynolds equation for a longitudinal component of velocity and turbulent energy equation.  However, in these equations, the number of unknowns greater than the number of equations. To obtain a closed system equations by following the from the paper G.S. Glushko [10] we introduce the semiempirical relations obtained by in the assumptions [11]:

1.        Transfer of the momentum by turbulent pulsations by diffusion of gradient type (Bussinesque hypothesis)

                                                                              (3)

where  coefficient of turbulent viscosity.

2.     Transferring the total of turbulent energy also carried out by the diffusion gradient type

                                                             (4)

where

 the summary diffusion coefficient.

3.        The process of dissipation of turbulence energy described by the relationship

                                                                                            (5)

where  the scale of turbulence;

 universal constant according to the [10],

Equations (3) - (5) include three empirical parameters and for determining which necessary to involve experimental results.

Using the results obtained in [10], which show that coefficient of eddy viscosity can be expressed as a function of turbulent Reynolds number  of writers [6] proposed another formula, which approximates the dependence of a turbulent viscosity:

                  (6)

Equation (6) agrees well with a piecewise smooth function, suggested in the article [10].

When calculating the coefficients in equation (6) were used the results of experiments [12] for circular tubes. For the summary diffusion coefficient the authors of [6] used the linear empirical dependence

                                                                                        (7)

where  constant coefficient. Quantity inverse is an analog of the turbulent Prandtl number.  According to the G.S. Glushko [10]  For the path length displacement for flow in a pipe (similar to the known formula Nikuradse) in [6] be used polynomial for a scale

                                                               (8)

Constants are determined from the empirical dependence for the resulting in G.S. Glushko [10] and from the Laufer’s experimental data [12]:  

Considering all the above, equation (2) and (1) can be transformed to the following form:

                                                     (9)

                                         (10)

where the coefficients and the scale are defined by (6) - (9) and averaging of signs omitted for simplicity. From the symmetry condition on the tube axis and the adhesion conditions of the liquid on the wall the boundary conditions written to (BC):

 under  and  under                         (11)

In general of BC (11) must be added the initial conditions (IC):

 under                                                               (12)

and set to change flow rate or the pressure gradient over time.

For the steady the periodic motion in a pipe IC (12) is not needed and the instantaneous values of flow or an average velocity in the cross section  are related to the pressure gradient. Indeed, using definition of the average velocity [7]:

                                                            (13)

and integrate the equation (9) over the radius of taking into account the conditions (11) and (13), we obtain:

                                                  (14)

where  wall shear stress,  Equation (14) is a special case depending on [7]:   without convective terms.

The continuity equation it follows that instantaneous values of the average velocity and flow rate for an incompressible liquid are identical in any cross section of pipe. Setting the law of variation or from the equation (14) we can find the pressure which in this framework will be the desired function. Conversely, setting the law of change of pressure gradient over time from (14) will be find  and  

The analysis of results. Given above system equations was solved numerical in at a given medium MathCAD harmonious law of change of rate  To confirm the effectiveness of both proposed model same, and calculation method were conducted the numerical calculations by the establish to a stationary flow the results are in satisfactory agreement with the experimental the data of F. Sedat Tardu,  Rogeiro Maestri and J. Laufer [1,12].

For nonstationary flow consumption was specified the change law of according a harmonious [7]:

                                                                     (15)

where average discharge;

 the relative amplitude of flow rate fluctuations;  constants given quantity​​. As well as in case of laminar pulsed flow a dimensionless criterion of characterizing relative influence of inertia and viscosity parameter is  and for the average of the turbulent flow - parameters  and  where

References

1.     F. Sedat Tardu,  Rogeiro Maestri. Wall shear stress modulation in a turbulent flow subjected to imposed unsteadiness with adverse pressure gradient. Fluid Dyn. Res. 42, 2010, 21 pp.

2.     Khaleghi, A., Pasandideh-Fard, M., Malek-Jafarian, M., Ghung, Y.M. Assessment of common turbulence models under conditions of temporal acceleration in a pipe. Journal of Fluid Mechanics, Vol. 3, No. 1, pp. 25-33, 2010.

3.     Zandi, I. and Govatos, G. Heterogeneous ow of solids in pipelines. ASCE J. Hyd. Div., 93, 1967, 145-159.

4.     Lazarus, J.H., Neilson, I.D. A generalized correlation for friction head losses of settling mixtures in horizontal smooth pipelines. Hydrotransport 5. Proc. 5th Int. Conf. on Hydraulic Transport of Solids in Pipes.,1, 1978,  B1-1-B1-32.

5.     Amies, G., Greene, B. Aircraft hydraulic systems dynamic analysis. Volume IV. Frequency response (HSFR). Wright-Patterson Air Force Base Technical Report AFAPL-TR-76-43, IV, 1977.

6.     Âàñèëüåâ Î.Ô., Êâîí Â.È. Íåóñòàíîâèâøååñÿ òóðáóëåíòíîå òå÷åíèå â òðóáå. – ÏÌÒÔ, 1971, ¹ 6.

7.     Ãëèêìàí Á.Ô. Ìàòåìàòè÷åñêèå ìîäåëè ïíåâìîãèäðàâëè÷åñêèõ ñèñòåì. – Ì.: Íàóêà, 1986. – 368 ñ.  

8.     Áóêðååâ Â.È., Øàõèí Â.Ì. Ñòàòèñòè÷åñêè íåñòàöèîíàðíîå òóðáóëåíòíîå òå÷åíèå â òðóáå. – Äåï. ðóêîïèñü, ÂÈÍÈÒÈ, ¹ 866-81, Íîâîñèáèðñê, 1981.   

9.     Ìîíèí À.Ñ., ßãëîì À.Ì. Ñòàòèñòè÷åñêàÿ ãèäðîìåõàíèêà. Ìåõàíèêà òóðáóëåíòíîñòè. ×. 1., Ì.: Íàóêà, 1965.

10.  Ãëóøêî Ã.Ñ. Òóðáóëåíòíûé ïîãðàíè÷íûé ñëîé íà ïëîñêîé ïëàñòèíå â íåñæèìàåìîé æèäêîñòè. – Èçâ. ÀÍ ÑÑÑÐ, Ìåõàíèêà, 1965, ¹ 4.

11.  Âàñèëüåâ Î.Ô., Àòàâèí À.À., Âîåâîäèí À.Ô. Ìåòîäû ðàñ÷åòà íåóñòàíîâèâøèõñÿ òå÷åíèé â ñèñòåìàõ îòêðûòûõ ðóñåë è êàíàëîâ / ×èñëåííûå ìåòîäû ìåõàíèêè ñïëîøíîé ñðåäû. – Íîâîñèáèðñê, 1975. Ò. 6, ¹ 4. 

12.  Laufer J. The structure of turbulence in fully developed pipe flow. – Nat. Advic. Com. Aeronaut., 1954, Rept. ¹ 1175.