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Turbulent flows generated/designed in multiscale/fractal ... - Ercoftac

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first session | Fundamentals<br />

Multi-scale Self-similar Coherent Structures <strong>in</strong> Developed Turbulence<br />

Susumu Goto<br />

Department of Mechanical Eng<strong>in</strong>eer<strong>in</strong>g, Okayama University, Okayama, 700-8530, Japan<br />

E-mail: goto@mech.okayama-u.ac.jp<br />

In order to reveal the coherent structures <strong>in</strong> fully developed turbulence and to understand their<br />

roles <strong>in</strong> the dynamics and statistics of turbulence, direct numerical simulations (DNS) of homogeneous<br />

isotropic turbulence <strong>in</strong> a periodic cube are conducted. By the DNS employ<strong>in</strong>g the Fourier spectral<br />

method with 2048 3 grid po<strong>in</strong>ts, turbulence at the Taylor-length based Reynolds number equal to 580<br />

is simulated.<br />

The multi-scale coherent structures are, then, visualised by the iso-surfaces of the coarse-gra<strong>in</strong>ed<br />

enstrophy, which is estimated by the low-pass filter<strong>in</strong>g of the Fourier components of the vorticity field.<br />

Results are shown <strong>in</strong> the figure below. It is clearly observed that thus visualised coherent vortical<br />

structures have ma<strong>in</strong>ly tubular shapes with radii of the order of the coarse-gra<strong>in</strong><strong>in</strong>g scale, whereas<br />

MONDAY<br />

their28 length<br />

MARCH<br />

is as long<br />

2011<br />

as the <strong>in</strong>tegral<br />

| 10.25-11.00<br />

length.<br />

This multi-scale self-similar coherent structures play roles <strong>in</strong> the turbulence dynamics. For example,<br />

the <strong>fractal</strong> structure of preferentially concentrated heavy small particles <strong>in</strong> turbulence is well described<br />

<strong>in</strong> term of these multi-scale coherent structures.<br />

It is also important to describe, based on these coherent structures, one of the most important<br />

dynamics of turbulence, i.e. the energy cascade. To <strong>in</strong>vestigate this process <strong>in</strong> detail, we <strong>in</strong>troduce<br />

(Goto 2008, JFM) scale-dependent energy and its transfer. It is, then, numerically verified that the<br />

Multiscale self-similar<br />

coherent structures <strong>in</strong><br />

developed turbulence<br />

energy at a scale (l, say) is conf<strong>in</strong>ed <strong>in</strong> the coherent vortex tubes at l, whereas the energy at scale l<br />

transfers (probably to smaller scales) the regions surround<strong>in</strong>g the vortex tubes at l, where the stra<strong>in</strong><br />

rate at the scale l is high. This result implies that the energy cascade is caused by the creation of the<br />

th<strong>in</strong>ner vortex tubes by the vortex stretch<strong>in</strong>g <strong>in</strong> larger-scale stra<strong>in</strong> field around fatter vortex tubes.<br />

Indeed, we can easily f<strong>in</strong>d the <strong>in</strong>vents which support this scenario of the energy cascade.<br />

Two problems arise from this conclusion, however. First one is on the universality of turbulence<br />

statistics, s<strong>in</strong>ce the above mechanism of the energy cascade implies that coherent structures at the<br />

Taylor micro scale can be directly created by the large-scale structures at the <strong>in</strong>tegral length. Secondly,<br />

to my knowledge, the relation between the Kolmogorov energy spectrum and this mechanics<br />

S. Goto<br />

of turbulent energy cascade is still open; where is the spiral structure, for example?<br />

Department of Mechanical Eng<strong>in</strong>eer<strong>in</strong>g, Okayama University, JAPAN<br />

Different ways of generat<strong>in</strong>g turbulence | SECOND session<br />

MONDAY 28 MARCH 2011 | 11.30-12.05<br />

Successful attempts of large<br />

scale-turbulence realization<br />

by a Makita-Type turbulence<br />

generator and a buoyant jet<br />

Successful Attempts of Large Scale-Turbulence Realization<br />

<strong>in</strong> a cross by a Makita-Type w<strong>in</strong>d Turbulence Generator<br />

and a Bouyance Jet <strong>in</strong> a Cross W<strong>in</strong>d<br />

N. Sekishta and H. Makita<br />

Toyohashi University of Technology, JAPAN<br />

Nobumasa SEKISHITA 1 and Hideharu MAKITA 2<br />

1,2 Toyohashi University of Technology<br />

(a) (b) (c) (d)<br />

FIG 1: Iso-surfaces of the enstrophy of the coarse-gra<strong>in</strong>ed enstrophy at (a) coarse-gra<strong>in</strong>ed 680η, (b) 340η (c) 170η and at (d)(a) 84η; 680η, where η is(b) the 340η (c)<br />

170η and<br />

Kolmogorov<br />

(d) 84η;<br />

length<br />

where<br />

scale. All<br />

η<br />

ofis these<br />

the<br />

scales<br />

Kolmogorov<br />

are <strong>in</strong> the <strong>in</strong>ertial range.<br />

length<br />

The sidescale. of the shown<br />

All<br />

cube<br />

of<br />

is 5400η<br />

these scales<br />

<strong>in</strong> (a,b,c), and 1700η <strong>in</strong> (d).<br />

are <strong>in</strong> the <strong>in</strong>ertial range. The side of the shown cube is 5400η <strong>in</strong> (a,b,c), and<br />

1700η <strong>in</strong> (d).<br />

In order to reveal the coherent structures <strong>in</strong> fully developed turbulence and to<br />

understand their roles <strong>in</strong> the dynamics and statistics of turbulence, direct numerical<br />

simulations (DNS) of homogeneous isotropic turbulence <strong>in</strong> a periodic cube are<br />

conducted. By the DNS employ<strong>in</strong>g the Fourier spectral method with 2048 3 grid<br />

po<strong>in</strong>ts, turbulence at the Taylor-length based Reynolds number equal to 580 is<br />

simulated. The <strong>multiscale</strong> coherent structures are then visualised by the isosurfaces<br />

of the coarse-gra<strong>in</strong>ed enstrophy, which is estimated by the low-pass<br />

filter<strong>in</strong>g of the Fourier components of the vorticity field. Results are shown <strong>in</strong> the<br />

figure. It is clearly observed that thus visualised coherent vortical structures have<br />

ma<strong>in</strong>ly tubular shapes with radii of the order of the coarse-gra<strong>in</strong><strong>in</strong>g scale, whereas<br />

their length is as long as the <strong>in</strong>tegral length. This <strong>multiscale</strong> self-similar coherent<br />

structures play roles <strong>in</strong> the turbulence dynamics. For example, the <strong>fractal</strong> structure<br />

of preferentially concentrated heavy small particles <strong>in</strong> turbulence is well described<br />

<strong>in</strong> term of these <strong>multiscale</strong> coherent structures.<br />

It is also important to describe, based on these coherent structures, one of the<br />

most important dynamics of turbulence, i.e. the energy cascade. To <strong>in</strong>vestigate<br />

this process <strong>in</strong> detail, we <strong>in</strong>troduce [9] scale-dependent energy and its transfer.<br />

It is then numerically verified that the energy at a scale (l, say) is conf<strong>in</strong>ed <strong>in</strong> the<br />

coherent vortex tubes at l, whereas the energy at scale l transfers (probably to<br />

smaller scales) the regions surround<strong>in</strong>g the vortex tubes at l, where the stra<strong>in</strong> rate<br />

at the scale l is high. This result implies that the energy cascade is caused by the<br />

creation of the th<strong>in</strong>ner vortex tubes by the vortex stretch<strong>in</strong>g <strong>in</strong> larger-scale stra<strong>in</strong><br />

field around fatter vortex tubes. Indeed, we can easily f<strong>in</strong>d the <strong>in</strong>vents which support<br />

this scenario of the energy cascade.<br />

Two problems arise from this conclusion, however. First one is on the universality<br />

of turbulence statistics, s<strong>in</strong>ce the above mechanism of the energy cascade implies<br />

that coherent structures at the Taylor microscale can be directly created by the<br />

large-scale structures at the <strong>in</strong>tegral length. Secondly, to my knowledge, the relation<br />

between the Kolmogorov energy spectrum and this mechanics of turbulent energy<br />

cascade is still open; where is the spiral structure, for example?<br />

Hibarigaoka 1-1, Tenpaku, Toyohashi, Aichi 441-8580, Japan<br />

Atmospheric boundary layers were seki@me.tut.ac.jp simulated <strong>in</strong> a laboratory w<strong>in</strong>d tunnel by<br />

regulat<strong>in</strong>g parameters of a turbulent shear flow generator. The generator has a<br />

shear Atmospheric flow device boundary and layers an were active simulated grid <strong>in</strong> with a laboratory agitator w<strong>in</strong>d w<strong>in</strong>gs tunnel driven by regulat<strong>in</strong>g by 40 parameters stepp<strong>in</strong>g of a<br />

motors. The generator could control turbulence characteristics; mean velocity<br />

turbulent shear flow generator. The generator has a shear flow device and an active grid with agitator w<strong>in</strong>gs<br />

U=0~8m/s, turbulence <strong>in</strong>tensity u’/U ∞<br />

=1~13% and <strong>in</strong>tegral scale L ux<br />

=0.02~1.9m.<br />

driven by 40 stepp<strong>in</strong>g motors. The generator could control turbulence characteristics; mean velocity<br />

Reynolds stress distributions were also <strong>in</strong>tensified throughout the thick boundary<br />

U=0~8m/s, layer by the turbulence present <strong>in</strong>tensity setup. The u'/Umaximum =1~13% and turbulence <strong>in</strong>tegral scale Reynolds L ux =0.02~1.9m. number, Reynolds R λ<br />

, reached stress<br />

distributions about 650 were at Ualso ∞<br />

=8m/s <strong>in</strong>tensified and throughout the spectrum the thick had boundary a wide layer <strong>in</strong>ertial by the sub present range setup. comparable<br />

The maximum<br />

turbulence to those Reynolds <strong>in</strong> natural number, atmospheric R , reached boundary about 650 layers. at U =8m/s and the spectrum had a wide <strong>in</strong>ertial<br />

subrange Coherent comparable structures to those were <strong>in</strong> natural <strong>in</strong>vestigated atmospheric <strong>in</strong> boundary a round layers. jet of heated air with temperature<br />

difference, Coherent structures 0, 20, were 40 and <strong>in</strong>vestigated 60K. The <strong>in</strong> a round present jet of heated jet was air with vertically temperature ejected difference, <strong>in</strong> a 0, cross 20, 40<br />

flow field. Three k<strong>in</strong>ds of flow pattern <strong>in</strong> the jet with smoke were observed by flow<br />

and 60K. The present jet was vertically ejected <strong>in</strong> a cross flow field. Three k<strong>in</strong>ds of flow pattern <strong>in</strong> the jet<br />

visualization <strong>in</strong> the cross flow <strong>generated</strong> with or without a turbulence grid. In the<br />

with smoke were observed by flow visualization <strong>in</strong> the cross flow <strong>generated</strong> with without a turbulence<br />

case of mode I, hairp<strong>in</strong>-type vortices occurred <strong>in</strong> the jet. Two vortex tubes with and<br />

grid. without In the strong case of mutual mode I, hairp<strong>in</strong>-type <strong>in</strong>teraction vortices (bifurcation) occurred <strong>in</strong> were the jet. <strong>generated</strong> Two vortex for tubes mode with II and and without III,<br />

strong respectively. mutual <strong>in</strong>teraction Vortex (bifurcation) behaviour, were the <strong>generated</strong> convection for mode velocity II and III, of the respectively. coherent Vortex vortices, behavior, the<br />

convection Strouhal velocity number, of the etc., coherent was vortices, <strong>in</strong>vestigated the Strohal from number, the results etc., was of <strong>in</strong>vestigated motion pictures from the results taken of<br />

motion by a high pictures speed taken camera by a high (1000frame/s). speed camera (1000frame/s). The convection The convection velocity velocity of the of the coherent<br />

structures structures decreased decreased with <strong>in</strong>creas<strong>in</strong>g with <strong>in</strong>creas<strong>in</strong>g the temperature the difference. temperature These vortex difference. shedd<strong>in</strong>g frequencies These vortex and the<br />

shedd<strong>in</strong>g frequencies and the Strouhal numbers decreased with <strong>in</strong>creas<strong>in</strong>g the<br />

Strohal numbers decreased with <strong>in</strong>creas<strong>in</strong>g the temperature difference.<br />

temperature difference.<br />

vortex formation region vortex region<br />

Y/D<br />

20<br />

10<br />

0<br />

flow<br />

0 20 40 60 80 100<br />

X/D<br />

Fig. 1. <strong>Turbulent</strong> Shear flow generator. Fig. 2 Vortex formation region and vortex region.<br />

6<br />

turbulent <strong>flows</strong> <strong>generated</strong>/<strong>designed</strong> <strong>in</strong> <strong>multiscale</strong>/<strong>fractal</strong> ways: fundamentals and applications<br />

turbulent <strong>flows</strong> <strong>generated</strong>/<strong>designed</strong> <strong>in</strong> <strong>multiscale</strong>/<strong>fractal</strong> ways: fundamentals and applications<br />

7

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