Differential equations for integral scales of semiempirical developed-turbulence тheory

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Автори: Karas, V.I., Maljkhanov, V.P.
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Опубліковано: Національний науковий центр «Харківський фізико-технічний інститут» НАН України 2000
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Цитувати:Differential equations for integral scales of semiempirical developed-turbulence тheory / V.I. Karas’, V.P. Maljkhanov // Вопросы атомной науки и техники. — 2000. — № 1. — С. 200-204. — Бібліогр.: 10 назв. —англ.

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Digital Library of Periodicals of National Academy of Sciences of Ukraine
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author Karas, V.I.
Maljkhanov, V.P.
author_facet Karas, V.I.
Maljkhanov, V.P.
citation_txt Differential equations for integral scales of semiempirical developed-turbulence тheory / V.I. Karas’, V.P. Maljkhanov // Вопросы атомной науки и техники. — 2000. — № 1. — С. 200-204. — Бібліогр.: 10 назв. —англ.
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container_title Вопросы атомной науки и техники
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fulltext 200 UDK 532.517.4 DIFFERENTIAL EQUATIONS FOR INTEGRAL SCALES OF SEMIEMPIRICAL DEVELOPED-TURBULENCE THEORY V.I. Karas’, V.P. Maljkhanov* National Science Center “Kharkov Institute of Physics and Technology”, Kharkov 61108, Ukraine, * CRYOCOR, Moscow 105043, Russia The calculation of turbulent shear flows and of turbulent diffusion in these flows calls for the theory that enables the anisotropic properties of the flows to be adequately taken into account. The information provided by classical semiempirical theories of Boussinesque, Prandtle, Taylor, Carman is limited to mere averaged velocities, and appears insufficient, as it gives no way of calculating the spatial and temporal distributions of turbulence intensity and turbulent diffusion coefficients. In this regard, of interest are the semiempirical theories, where in parallel with the Reynolds equations use is made of the equations for turbulent characteristics, in particular, the turbulent energy (b)-balance equation [1]. Similarly to classical semiempirical theories, these theories also comprise the notion of the coefficient of turbulent diffusion for different substances (momentum, energy, etc.), however, the dependence of this coefficient on statistical characteristics of turbulence is quite different and is based on the following obvious considerations. It is known that the kinematic coefficient of molecular viscosity is related to the average molecular velocity Um and the average free path length of molecules lm by v=Umlm. It can be assumed that the coefficients of turbulent viscosity would be described by similar relations, where the corresponding characteristics of disordered turbulent flows will play the role of molecular flow characteristics Um and lm. Thus the mean-square value of pulsation velocity, i.e., √b, is obviously analogous to Um. Instead of lm, one should use the turbulence scale l, i.e., the length dimensionality describing the mean distance that the turbulent formations can be displaced without disturbing their individuality (i.e., the Prandtle “way of mixing”, which is coincident in the order of magnitude with the “correlation length” calculated from the spatial correlation function). In this case, the anisotropic turbulence can be characterized by different scales in different directions. At the same time, it is the semiempirical theories that are now gaining acceptance [2]. In these theories, the anisotropy of the flow can be considered in terms of pulsation velocity components, differing in direction, but at one (isotropic) scale. The very construction of the semiempirical theory in this way shows its limited usefulness, because in reality the anisotropy in shear flows must exert an effect not only on pulsation velocity values, but on the scales as well. Strictly speaking, at each point of the flow, along with the pulsation velocity components, a scale ellipsoid must be determined, i.e., a symmetric second- rank tensor lij (scale tensor) must be assigned, the components of which have the length dimensionality. Therefore, to hold the rigidity in the determination of anisotropic properties of the flow, one needs not only the equations for the pulsation velocity components but also the equations for turbulence scales; however, this will result in a bulky set of equations. The set of equations for turbulence energy and scales may appear more compact to consider the anisotropic properties of flows. Then the tensor of turbulent viscosity coefficients can be expressed as ij ijv bl= (1) This approach appears more natural, because the turbulence energy is the parameter quite real for shear flows. With the tensor vij, we can express the Reynolds stresses in terms of the turbulence energy, scales and derivatives of averaged velocities, assuming (as is generally the case) that the dependence of these stresses on the derivatives ∂Ui/∂xj is linear, namely, ( )2 1 3 2i j ij i j j iu u b b l lα α α αδ= − Φ + Φ (2) where ji ij j i UU x x ∂∂ Φ = + ∂ ∂ is the strain tensor, Ui is the ith pulsation velocity component value, Uj is the jth averaged velocity component value, δij is the Kronecker symbol, <...> is the probability-theoretic averaging. This formula was proposed by Monin [3]. It explicitly takes into account the symmetry of the Reynolds stress tensor, yet it often neglects the significant fact that generally (except for the isotropic turbulence) normal stresses differ between themselves in magnitude. In a number of cases, one can simply take as a first approximation that lij = lδij is the isotropic tensor, i.e., take the hypothesis expressed by the formula 2 3i j ij iju u b l bδ= − Φ (3) as the base (the Reynolds stress tensor just the same remaining anisotropic). It should be noted that in the literature, because of the lack of data on the scale tensor lij, it is formula (2) that is used to calculate turbulent flows by the set of equations including the turbulent energy equation. If the use is made of the common hypothesis that the turbulent diffusion coefficients of different substances are equal to the turbulent viscosity coefficient to an accuracy of numerical factors, then the introduction of the tensor lj allows one to write in terms of principal unknowns (e.g., 201 [4]) both the third moments of the velocity field 1 2 i b i a b u u u bl xβ β αα ∂ = − ∂ (4) (where bα is a certain numerical coefficient) and the density components of the turbulent impurity flow i i a u bl xϑ αϑ α ∂Θ = − ∂ (5) where ϑ is the concentration pulsation, Θ is the concentration average. The construction of closed semiempirical theory of inhomogeneous turbulence around the set of Reynolds equations, the continuity equation and the turbulent energy-balance equation calls for the presence of data on space-time variation of scales, that cannot be obtained from the principal equations of the set. These data can be obtained either by processing the experimental data or by solving differential equations for scales. Currently some studies have been advanced, which propose the equations for scales. Let us consider a homogeneous isotropic turbulence, for which all points and directions are of equal importance, therefore, all single-point characteristics are constant in space. In this case, two integral scales are of importance: longitudinal Λf and transverse Λg. They are expressed in terms of longitudinal and transverse correlation coefficients f(x) and g(x) by the following formulas ( ) 0 g g x dx ∞ Λ = ∫ , ( ) 0 f f x dx ∞ Λ = ∫ , (6) However, in the consideration of inhomogeneous nonisotropic turbulence these definitions become meaningless because of nonequivalence of different points and directions in the flow. Generalizing the isotropic case, Rotta [5] has defined the “averaged scale” of turbulence L by the following relationship ( ) ( ) ( ) 0 3 , , , 8 , dk L x t F k x t b x t k π ∞ = ∫! ! ! , (7) where k is the wave vector modulus, x → is the radius vector of the point under consideration, ),,( txkF → is the function of three-dimensional spectrum (sum of diagonal elements of the spectral function tensor, integrated over all possible directions of the wave vector → k ). The differential equation derived for the thus introduced “average scale” inadequately describes its behavior in the vicinity of a hard wall. In [6], Glushko has eliminated this drawback by modifying formula (7) relationship ( ) ( ) ( )2 2 2 1 2 3 2 2 , ,3 , , , 16 , x x Q x t L x x x t d b x t ξ ξ π ξ ∞ ∞ −∞ − −∞ = ∫ ∫ ∫ !! ! ,(8) where Q is the half-sum of diagonal moments of the correlation function tensor for the points 2 x ξ− ! ! and 2 x ξ+ ! ! . The physical meaning of the modification consists in the explicit consideration of the condition of attachment on the wall (mathematically, this means the restriction of the region of variation ξ → ). Expressions (7) and (8) are equivalent at the centre of the flow. In fact, as ),,( txQ →→ ξ is essentially different from zero for  → ξ  <L, then at x2 >>L (this holds at the centre of the flow) the upper and lower limits can be considered infinite, and thus the restriction on possible → k values is removed. Note that formulae (7) and (8) take into account only the inhomogeneity of the flow, leaving quite apart its anisotropy. This situation is not wholly satisfactory, because turbulence can be characterized by different scales in different directions. The flow anisotropy can be taken into account by introducing the scale tensor. Here, of importance is the issue which interpretation should be given to these scales. If the coordinate frame is chosen so that only diagonal components of the scale tensor are nonzero, then each principal direction in space has the sole scale. Apparently, in the determination of these tensor components one can proceed from the following qualitative considerations: • the scale in the given direction must characterize the same-direction correlation of both longitudinal and transverse components of pulsation velocity; • the scale must make allowance for the presence of flow-limiting surfaces, on which the averaged velocity and the pulsation velocity become zero; • in the case of isotropic homogeneous flow, the scale must be coincident with either transverse or longitudinal integral scale. In view of the mentioned requirements, let us define the scale in the direction xi as a mean integral scale of correlation between like pulsation-velocity components in the given direction, i.e., ( ) ( ) ( ) ( ) ( )( ) 3 1 3 1 , , , 8 , 2ii kk kx i l x t R x t d b x t δ ξ ξ ξ δ ξ=Ω = ∑∫∫∫ ! ! ! !! ! ! ,(9) where b is the specific turbulent energy, Ω (x) is the domain of ξ variation * 2 2ij i j j iR u u u x u x ξ ξ′ ′= = − +           ! ! ! ! , ( )1 2 3, ,ξ ξ ξ ξ= ! is the distance between the points under consideration, )()()()( 321 → = ξδξδξδξδ is the Dirac delta function having the following property ( ) 1d ε ε δ ξ ξ − =∫ , where 0ε > . We now show that this definition of lij in the 202 case of isotropic homogeneous turbulence is coincident with the definition of the transverse integral scale Λg. It is known that for the turbulence of this kind ( ) 2 2 3ij i j ij f g R b gξ ξ ξ δ ξ − = +     ! , where f and g are, respectively, the longitudinal and transverse correlation coefficients, ijδ is the Kronecker symbol. Taking the half-sum of diagonal elements of the tensor Rij and making use of the known relationship [7] between f and g, we obtain ( ) 3 1 1 3 2 3kk k b f R fξ ξ ξ= ∂ = + ∂       ∑ ! ! ! , and since i i f fξ ξ ξξ ∂ ∂= ∂∂ ! ! , then ( ) ( ) 2 1 3 8 1 3 8 ii i i i i i i f f d f f d l ξ δ ξ ξ ξ ξ δ ξ ξ ξ ξ ∞ ∞ ∞ −∞ −∞ −∞ ∞ −∞ ∂ = + = ∂ ∂ = + ∂            ∫ ∫ ∫ ∫ ! ! ! Taking into consideration that f is the even function of ξi, we find ( ) 0 0 1 3 4 3 1 4 2 ii i i i f f g i i f l f d f d ξ ξ ξ ξ ξ ∞ ∞ ∂ = + = ∂ Λ − Λ = = = Λ −               ∫ ∫ , where Λf(g) is, respectively, the longitudinal (transverse) integral scale. By definition (9), the functional dependences of lij on the coordinates can be obtained in three ways, namely: - from the experimental data on correlation functions; - with the use of theoretical dependences for correlation functions; - by equations formed for lij. Let us illustrate the first way of setting up functional dependences lij on the coordinates using the experimental data of Conte-Bellaux [8] who measured, among other important turbulence characteristics, the spatial distributions of turbulent energy b in the plane flow, the average squared components of pulsation velocities 〈ui 2〉 , the correlation coefficients ( ) ( ) ( ) ( ) ( ) 1 2 3 1 2 3 2 2 1 2 3 1 2 3 , , , , , , 0, 0 , , , , i j ij i j u x x x u x x x r x u x x x u x x x γ γ γ + = + ! As is seen from expression (9), the calculation of lij requires the correlation functions of the form ( ), 2 2 ij j iR x u x u x ξ ξ ξ == − +           ! ! !! ! ! . They can easily be related to the correlation coefficients rij(x,ξ) measured in experiment, namely: ( ) ( ) ( ) ( ), , 0 , 0 , 2 2 2 ee ee ee ee R x R x R x r x ξ ξ ξ ξ ξ= − + − ! ! ! ! !! ! ! ! . Since the experiment was conducted in the plane flow, all single-point characteristics, including lij , are merely the functions of one coordinate x2 (the axis x2 is directed along the averaged velocity variation), and for two-point characteristics the dependence on the first argument is related only to the function of x2. The experimental data were used to plot ( ) ( ) 3 1 1 , 2 kk i k R x b xξ = ∑ ! ! versus  ξi  for different x2/D values (where D is the half-width of the channel). Finding the area under the curve (e.g., with a planimeter) that corresponds to the direction i and to a certain x2/D value and multiplying by a constant factor, we obtain the 2 ii x l D     values. Based on the definition (1) and the data obtained, one can ascertain the known fact about the excess of the longitudinal coefficient v11 over the transverse coefficient v22 by factors of about 3 to 4. For comparison, the data measured by Conte- Bellaux are used for the correlation lengths defined as It should be noted that the definition (10) provides a consideration of correlation in one direction only, this being insufficient for finding the diagonal elements of scale tensor, as two of the scales must characterize certain “averaged correlation lengths” in transverse directions, and this is not provided by the definition. Besides, it masks the anisotropy of the flow, because even in the case of homogeneous isotropic turbulence the correlation length L1 will be twice as large as the lengths L2 and L3. Using the introduced integral turbulence scale (9) as the base, differential equations can be set up to take into account the anisotropic properties of the flow. In the derivation of equations for diagonal components of integral scale tensor (DCIST), according to (9), we use the equation for ),,( txQ →→ ξ , that is found by folding the equations for two-point moments Rij), multiply it by 3/8 ( , )b x t → and integrate over )( → Ω x .In the integration one should take into account that the average velocity and the pulsation velocity are equal to zero at the boundary of the region. It is assumed that all two-point characteristics are dependent on the ratio ξi/li      → tx, . Then, similarly to [2,5], we write down each 203 characteristic as follows: ( ) ( ) ( ) 1 2 3 11 22 33 , , , 0, , ,x t x t f l l l ξ ξ ξ ξ ΓΓ = Γ      !! ! , where f(r) satisfies the condition ( ) ( ) ( ) ( )( ) ( )3 8 , x i f d Const b x t δ ξ ξ ς δ ξ Γ Γ Ω = =∫∫∫ ! ! ! ! . This means that the dependence on the direction in space is determined by the dependence on lii( tx , → ). The mentioned manipulations lead to the set of equations for b lii( tx , → ). ( ) ( ) ( ) ( ) ( ) ( ) ( ) , 0, , 0, ii ii i k ki ki ii k k b bii ki ki ii k k s s ii t bl bl U U R x t l t x x bl v I x t l x x T l ς ς ς ε ∂ ∂ ∂ + + = ∂ ∂ ∂ ∂∂ = + + ∂ ∂ + −       ! ! , (11) ( ) 3 2 1 1 ik i k s ii i i k ikkk ii ii T vbl fl l l δ β α ξ ξ δ= − + = − +                        ∑ , i Sξ ∈ (12) where v is the kinematic viscosity coefficient; ςkiς(b) kiςs, αk, βi are the constants, S is the surface of the region Ω , ( ) ( ) 2 / 2b k k i i kI u u u pu ρ = + , p - p is the pressure pulsation , 2 i t k u v x ε ∂ = ∂      . The turbulent energy balance equation has the form ( ) ( ) ( ) , 0, , 0, i k ki k k b ki t k k b b U U R x t t x x b v I x t x x ε ∂ ∂ ∂ + + = ∂ ∂ ∂ ∂ ∂ = + − ∂ ∂       ! ! . (13) To derive equations for DCIST, we need only take the difference between (11) and (13) multiplied by lii and transform it in accordance with the above-given closure hypotheses. In the general case, to calculate the turbulent shear flow, the derived equation should be solved along with the equation for averaged velocities and turbulent energy. Besides, it is essential to determine the unknown constants entering into the closure equation. Further, we consider experimental studies of a steady-state plane-parallel turbulent flow between two walls spaced at 2D. For convenience, we transform the problem into a formally nonstationary task with the boundary conditions 0il E y y ∂ ∂ = = ∂ ∂ at y=1 (middle of the flow) il =E=0 at y=0 (wall) where 2x y D = , ii i ll D = , 2 f bE U = , fU t t D ′ = , Re fU D ν = is the analog of the Reynolds number, Uf is the dynamic velocity. Along with the boundary conditions, we assign the initial conditions for li, E, approaching the experimental values obtained from ref. [7] by means of corresponding transformations. Using the physical properties of the plane-parallel shear flow with respect to the balance between the terms of turbulent energy equation, and based on the initial values for li and E, we obtain the constants klσ , 3σ , c , æ , ( )bα , ( )b kς , δ , iβ , kα . The set of equations was solved by the finite- difference method using the implicit scheme. At each time step, four equations for li and E are solved. The equations are solved by the method of matrix run [7-8] with the use of the Samarsky difference scheme for solving parabolic-type quasilinear equations [9]. The DCIST and E values, found at each time step, are used to calculate the related coefficients of difference equations; the calculations are repeated in the same sequence until the steady-state profiles for li and E are obtained. In calculations, the following constant values were used: 0.15δ = ; 3.93c = ; æ=0.06 ; ( ) ( ) 3 1 1 , 2 kk i k R x b xξ = ∑ ! ! ; 12 0.21σ = ; 3 0.2σ = ; 1 0.1β = ; 3 0.42β = ; 2 0.16α = ; ( ) ( )2 20.6 0.000098 120b zα = − − , 2 50, 0.1 500 , 0.1 0.25 120, 0.25 y z y y y ≤ = < < ≥     3 2 2 2 2 y l f l y =           . With these values, the functional dependences for the DCIST were found. They were compared to the dependences plotted using the experimental data from ref. [7]. Comparison was also made between the bution of the turbulent viscosity coefficient ( )11 222T b l l δ ν = + , the experimental distribution plotted in [10] by the data of Lauder and Nunner for the flow in the tube, and also the function for the velocity deficit 1 0 f U U U − based on the Conte-Bellaux data [10] (where U0 is the velocity in the middle of the flow). The comparison of calculated results with the measured data shows that the proposed model provides a fair description of the turbulent shear flow. 204 References 1. А.S.Моnin, А.М Yaglom. Statisticheskaya gidromekhanika. - М.: Nauka, 1965. Part. 1. 2. J.C.Rotta // Z.Phys. 1951. vol. 129, p. 547; 1951. vol. 131, p. 51. 3. Тurbulentnye techeniya / Sbornik nauchnykh trudov. - М.: Nauka, 1970. 4. А.Т.Оnufriev // PMTF. 1970, т. 2, c. 62. 5. J.C.Rotta // Z. Angew. Math. Mech. 1970, vol. 50, p. 204. 6. G.Cont-Belaux. Тurbulentnoye techenie v kanale s parallel`nymi stenkami. - М.: Мir, 1968. 7. О.S.Маzhorova, Yu.P.Popov // Preprint IPM im. М.V.Кеldysha АN SSSR №134, 1974. 8. О.S.Маzhorova, B.N.Chetverushkin // Preprint IPM im. М.V.Кеldysha АN SSSR №29,1973. 9. A.А.Samarsky. Vvedenie v teoriyu raznostnykh skhem. - М.: Nauka, 1971. 10. I.О.Khintse. Тurbulentnost`. - М.: Physmatgiz, 1963.
id nasplib_isofts_kiev_ua-123456789-81669
institution Digital Library of Periodicals of National Academy of Sciences of Ukraine
issn 1562-6016
language English
last_indexed 2025-11-30T12:37:23Z
publishDate 2000
publisher Національний науковий центр «Харківський фізико-технічний інститут» НАН України
record_format dspace
spelling Karas, V.I.
Maljkhanov, V.P.
2015-05-19T08:37:43Z
2015-05-19T08:37:43Z
2000
Differential equations for integral scales of semiempirical developed-turbulence тheory / V.I. Karas’, V.P. Maljkhanov // Вопросы атомной науки и техники. — 2000. — № 1. — С. 200-204. — Бібліогр.: 10 назв. —англ.
1562-6016
https://nasplib.isofts.kiev.ua/handle/123456789/81669
532.517.4
en
Національний науковий центр «Харківський фізико-технічний інститут» НАН України
Вопросы атомной науки и техники
Нелинейные процессы
Differential equations for integral scales of semiempirical developed-turbulence тheory
Article
published earlier
spellingShingle Differential equations for integral scales of semiempirical developed-turbulence тheory
Karas, V.I.
Maljkhanov, V.P.
Нелинейные процессы
title Differential equations for integral scales of semiempirical developed-turbulence тheory
title_full Differential equations for integral scales of semiempirical developed-turbulence тheory
title_fullStr Differential equations for integral scales of semiempirical developed-turbulence тheory
title_full_unstemmed Differential equations for integral scales of semiempirical developed-turbulence тheory
title_short Differential equations for integral scales of semiempirical developed-turbulence тheory
title_sort differential equations for integral scales of semiempirical developed-turbulence тheory
topic Нелинейные процессы
topic_facet Нелинейные процессы
url https://nasplib.isofts.kiev.ua/handle/123456789/81669
work_keys_str_mv AT karasvi differentialequationsforintegralscalesofsemiempiricaldevelopedturbulencetheory
AT maljkhanovvp differentialequationsforintegralscalesofsemiempiricaldevelopedturbulencetheory