Visualization and LASER measurements on flow field and sand movement on sand dune

Size: px
Start display at page:

Download "Visualization and LASER measurements on flow field and sand movement on sand dune"

Transcription

1 Visualization and LASER measurements on flow field and sand movement on sand dune Yusuke Sakamoto¹, Daisuke Aoshima¹, Itsuki Nakamura¹, Takahiro Tsukahara¹, Makoto Yamamoto¹, Yasuo Kawaguchi¹ Department of Mechanical Engineering, Tokyo University of Science, Chiba, Japan, Abstract The installation of obstacles around sand dune is one of the promising methods to suppress sand movement. We focus on the effect of a small fence installed on a sand dune to clarify the mechanism of the sand movement. A model dune was installed in a horizontal wind tunnel. The flow field around the dune and the process of sand movement were measured using some laser systems, such as LDV, PIV and laser-sheet visualization. In our previous study, the effects of fence height and position on a dune erosion were investigated. A non-porous fence suppressed sand movements upstream of fence, but enhanced if downstream of the fence. The intensive erosion downstream of the fence was caused by separated shere flow from the edge of the fence. In the present study, the influence on flow and erosion by fence porosity was discussed. Four types of porosity were tested:, 1, 3, 5% open area. The shapes of eroded sand dunes were founded to depend on the porosity rate. The relationship between the sand dune erosion and the flow field around the dune was described with schematic diagrams. The flow around a fence on a flat plane was measured by PIV. It can be seen the scale and number of vertices from the edge of the fence were significantly different depending on the fence porosity. The critical friction velocity, which was estimated from the equation proposed by Shimazu et al. (28) and the velocity along the plane surface were compared. According to the present results, the porous fence is effective to suppress the sand movement downstream of the fence. It is found that the effective fence porosity for dune erosion depends on the fence condition. 1. Introduction The dynamics of sand particle in atmosphere have been investigated for many years with the aim of combating the desertification. The desertification is one of serious world-wide environmental problems. One of the main causes of the desertification is wind-blown sand movements in desert. This phenomenon occurs as a result of complicated combinations of various conditions such as sand-dune surface, ambient air flow, sand particles, and so on. This phenomenon is supposed to be the most significant source which gives rise to sand storm and yellow dust, and it finally induces more desertification, health damage and aerial pollution. Hence it is important to clarify the mechanism of the wind-blown sand movement. Many researchers have studied on the dynamics of sand dunes. For example, Bagnold (1956) classified types of sand movement in atmosphere into three: saltation, suspension, and surface creep. In their study, a critical friction velocity was introduced as threshold of an air-flow velocity about sand movement. When an air-flow velocity becomes higher than the critical friction velocity, sand particles start to move. Walker & Nickling (23) measured flow field behind a dune with numerical calculations. Andreotti et al. (22) investigated surface waves on the barchans, which were generated by dune collisions and changes in wind direction. In desert, the installation of obstacles around sand dunes is a promising method to suppress sand movements. The sand movement depends on the flow conditions of sand surface, the air-flow velocity and its fluctuation near the sand bed. Therefore, an obstacle installed on the sand bed can be expected to play an important role in the control of the flow field near the sand-dune surface. For example, sandbags, paving, planting, and fences have been proposed as the obstacles. Sakamoto et al. (25) researched the effect of a wind-break fence, which was framed with log on the top of an artificial embankment. Li et al. (22) used the method of straw checkerboards and planting xerophytic shrubs to fix sand dunes. There also exist some researches on effects of obstacles, such - 1 -

2 as a fence, on sand movements in desert. The validity of them has been confirmed, but a mechanism of this phenomenon has not been completely analyzed. Kim & Patel (2) and Lee and co-workers (1998, 21, 22) investigated the effect of a porous wind fence, the height of which was the same level as that of a relevant dune, on the wind erosion of the dune. However it is practically difficult to apply such a fence to real scale, since an actual sand-dune height is often over 3 m. Hence, we have studied the erosion of a sand dune, on which a small fence is installed. In our previous study, we investigated the effect of a small fence on wind-blown sand movements on a sand dune. The process of erosion was found to depend on the position and height of the fence. The dune erosion was suppressed in the upstream of the fence, but enhanced in the downstream of the fence. When a non-porous fence was installed at the top of the dune, sand movement was hardly occurred. On the other hand, the sand dune with a fence installed at the toe of the dune was collapsed drastically. It can be believed that the complicated flow behind the fence is accompanied by strong turbulent motions with a separated shear layer as well as a turbulent boundary layer and that the turbulent flow field should have close relation with the sand erosion. Thus it is important to suppress the separated flow, which induces high turbulent intensity. If the sand movement downstream of a fence is suppressed, the fence installed at the toe of the dune becomes more effective to avoid the strong erosion of the dune. In this study, we employed a porous fence to suppress the separated flow from the fence edge. The effect of porosity rate on the flow field around the fence and sand movement was also studied. To analyze the relationship between flow field and sand movement, a process of sand-dune erosion and a flow field around the fence were investigated with laser systems: i.e. laser-sheet visualization, laser-doppler velocimetry (LDV), and particle image velocimetry (PIV). 2. Experimental set up The experimental set-up is shown in Fig. 1. The blower and rectification part was 2.91 m long, and its internal dimensions at the outlet were mm 2. The maximum air velocity was 2 m/s, and its minimum relative turbulence intensity was.5%. The developing section was 1. m long, and the test section was 3. m long. The spanwise width of each section was 25 mm, and the upper surface of both sections was movable. The developing section in the upstream of a test section provides variety of turbulent intensity and scale by setting several roughness blocks on the bottom plate. The test section was equipped with the measuring windows for illuminating laser beams and taking pictures. A model dune was installed at 5 mm downstream from the entrance of the test section. For the observation of sand deposition and erosion, the model dune itself was made of sand. The nominal mean sand-particle diameter was 115 µm, which was categorized into the saltation type of sand movement under the present range of the wind velocity. The initial shape of model dune was triangular prism as shown in Fig. 1. This shape was chosen as a typical shape of an actual dune in desert. Owing to the temporal change in the dune shape, it was essential that another non-erosive model dune should be applied to investigate the flow field around the dune. The other model dune was build with metallic boards for measuring mean velocities and turbulent intensities around the model dune. The coordinate parallel to the upstream-side dune surface was named x l. The fence height was 2mm, which corresponded to 1/4 of the height of the dune, and was installed at only x l = 1 mm. We tested four types of porous fences, which had different porosities: ε = % (nonporous fence), 1%, 3%, and 5%. These fences had a geometric porosity, and the porosity rate was defined based on the area ratio of the pore of the fence. The porosity rates and the pore diameters of the fences we used are listed in Table 1. The approaching mean air velocity was fixed at 7.1 m/s

3 y Fence 8 mm x l x Model dune (Sand or metal) mm y x Blower and rectification part Developing section 1 mm Test section 3 mm Fig. 1 Experimental set up. Fig. 2 Measurement points for LDV. Table 1: Specification of porous fence Porosity ε Pore diameter d Pitch p 1% 1.8 mm 3% 3.1 mm 5% 4. mm 5. mm The air-flow velocity around the dune surface was measured by laser-doppler velocimetry (LDV) system. The two-color four-beam LDV system (Dantec dynamics, Co.) was employed in the back-scatter mode with a 3 mm focal-length lens and equipped with a 1. W argon-ion laser (Coherent, Co.: INNOVA 38C). Table 2 shows the specification of the LDV system in detail. The oil mist with a mean diameter of 1~3 µm was employed as tracer particles. The LDV probe was fixed on a two-dimensional traverse system. Note that LDV measurement was made only for the metallic prism (without erosion), which simulates the initial stage of the model sand dune. Figure 2 shows the measurement points around the model dune. Two kinds of arrangements of points were applied: one of them was in a wide area above the model dune, and the other a narrow area but with a fine resolution only behind a fence. It is known that a reattachment point in a separate flow behind a fence oscillates periodically. The present data were averaged for 1 seconds to obtain a temporalaveraged velocity. The velocity and turbulent intensity were calculated by a burst spectrum analyzer (Dantec dynamics, Co.: 57N21 BSA enhanced master). The shape of the dune surface was obtained by laser-sheet visualization technique. In this method, a laser sheet irradiates the sand-dune surface so that the measurement line can be detected, as illustrated in Fig. 3. The laser-sheet thickness and its spread angle are 5 mm and 4, respectively. Table 3 shows the specification of the visualization system in detail. Figure 4 displays a typical snapshot of the irradiated sand dune at the beginning of flow, in which the blue line was measured. The initial shape of the sand dune is shown by a dotted line. Such pictures were taken during experiments with blowing wind, and local heights of dune surface were drawn from the measurement lines. These pictures were taken by the single-lens reflex camera (Nikon, Co.: D6)

4 y x Laser sheet Camera z Dune Fig. 3 Schematic illustration of the experimental set-up of dune visualization. Fig. 4 Sand dune irradiated by laser sheet. Table 2 Specification of LDV system. Model INNOVA 38 C Output (maximum) 5.23 W Output (as use) 1. W Beam diameter 1.8 mm Wave length 488 nm, nm Focal length 31 mm Beam intersection angle 6.99 Measurement volume diameter 91 µm Measurement volume length 1.49 mm Table 3 S system. Inpu Spre Thickn The effective pixels of this camera was 1.2 million. The time from the beginning of each test is denoted as t (t =.5, 1, 2, 3, 4, 5, 6, 7, 8, 9, 1 min.). Before the blowing wind with an aimed velocity (t < ), a wind speed was well below a threshold value, at which the wind first starts to move the sand grains. At low wind speeds, no sand movement was observed. In order to obtain the detailed flow field influenced by a fence, a two-dimensional measurement of flow field around the fence on flat plane was conducted with a two-frame PIV system, as shown in Fig. 5. Table 4 shows the specification of the PIV system in detail. The oil mist was employed as tracer particles. The PIV system consisted of a double-pulse laser, laser-sheet optics arrangement, CCD camera, synchronizer, and computer for image-sampling and processing. The double-pulse laser (Litron Lasers, Co.: Nano S 65-15) was a combination of a pair of Nd:YAG lasers, each having an output of 4 mj/pulse and the wavelength of 532 nm. The pulse interval was set at 1 µs. The system was able to obtain 5 sets of images per second. The laser sheet thickness can be modified by adjusting the combination of cylindrical lenses. In this experiment, the laser-sheet thickness and the spread angle were set to be mm and 2, respectively. The CCD camera had a resolution of pixels and its pixel pitch was of µm. The camera lens was a 5 mm focal length and an aperture of 2.8. The picture frame size is mm 2. The sets of two pictures were analyzed with software (Dantec dynamics, Co.: Dynamic Studio). Incorrect vectors were reject and replaced through the following process. First, vectors, which were outside a certain range, were rejected. This range was determined from two components velocities and length of vectors in the flow condition. Next, the blank points were replaced by vector estimated from surrounding vectors. In this experiment, a total of 6 instantaneous velocity vector fields were acquired at each condition. The mean velocity fields were obtained by ensemble averaging the 6-4 -

5 Table 4 Specification of PIV system. Model Nano S Laser Nd: YAG double pulse Output (maximum) 4 mj / pulse Flow Laser sheet Wave length Pulse interval 532 nm 1 µm Measurement area Pulse duration 5 ns Spread angle 2 y Fence Camera resolution Focal length pixels 5 mm x Bottom plane of wind tunnel Fig. 5 Measurement area for PIV. Fig. 6 Flow field around dune: (a), (b), distribution of mean streamwise velocity; (c), (d), distribution of streamwise turbulent intencity. (a), (c) and (b), (d) non-porous fence and porous fence (e = 3%), respectively. instantaneous velocity vector fields on the grid points (63 63 grids). 3. Result and discussion Flow Field around Dune First, we present the measured air-flow field around the model dune with a fence and discuss the difference between a non-porous fence and a porous fence (ε = 3%). Figure 6 shows the distributions of the two quantities for each condition in the fence porosity: the streamwise mean velocity (U) in the left column of the figure; the streamwise root-mean-square (RMS) values (Urms) in the right column. The fence was installed at 1 mm from the toe of the dune (x l = 1 mm). When the non-porous fence was installed, there existed a reverse flow behind the fence, see Fig. 6(a). In such a flow, sand which were carried from downstream side accumulated near the fence of - 5 -

6 y/h x (mm) y/h 1 min 5 min.4.5 min 1 min 6 min 7 min.2 2 min 3 min 8 min 9 min 1 4 min 1 min 2 x (mm) 3 4 Fig. 7 Temporal evolution of dune surface with non-porous fence. Fig. 8 Temporal evolution of dune surface with porous fence (ε = 3%). y/h Initial shape ε = % ε = 1% ε = 3% ε = 5% x (mm) Fig. 9 Shapes of dune surface with fence at 1min. after from the beginning of air flow. the reverse-flow area. The downstream of the reverse-flow area, the fast favorable flow came over the fence existed. The flow velocity was enough to move sand away. Along border between the reverse flow and the favorable flow, there was a high turbulent intensity region by separated shear flow from edge of the fence. The region spread downstream along the dune surface. On the other hand, bottom counters show the flow field around dune installed a porous fence (ε = 3%). In this condition, the value and area of turbulent intensity of the shear separated flow was small. Especially the value along the dune surface was remarkably small compared with the case of nonporous fence. There wasn t a reverse flow and a calm slow flow existed downstream of the fence. It should be noted that there existed a high turbulent intensity area just behind the fence. According to these features, it seems that the process of dune erosion change with fence porosity. Dune-Erosion Process We measured the processes of erosion, i.e., temporal deformation of the dune shape, with emphasis on the influence of the installed fence. We employed four types of porous fences, which had different porosities: from % (normal plate without permeability) to 5%. At first, we will discuss the influence of the fence porosity rate ε on the process of the sand-dune erosion. Figures 7and 8 show typical evolutions of a sand dune in two cases, where a fence of a normal plate (ε = %) or a porosity fence (ε = 3%) was located at x l = 1 mm, until 1 minutes - 6 -

7 High turbulent intensity region Main flow Initial dune surface Fence Area3 (a) Area1 Area2 Eroded surface Flow through fence Main flow Fence Area4 (b) Area2 Calm region Area3 Fig. 1 Schematic diagram of the flow field in the downstream of a fence: (a) non-porous fence, (b) 3% porosity fence..42 Fig. 11 Mean stream lines and distribution of U rms around fence on flat plane: (a) non-porous fence, (b) ε = 1%, (c) ε = 3%, (d) ε = 5%. after from the beginning of the test. When the non-porous fence was applied, the top of the dune was subjected to intensive erosion, as given in Fig. 7. In the area of downstream of the fence, the sand dune was eroded constantly in the first few minutes. However, when the top of the sand dune became low as the height of the fence, the erosion had calmed down. At 1 min from the beginning of the test, the dune took the form of a trapezoid. On the other hand, when the 3% porosity fence was installed, the erosion around the top of dune was mild, and thereby the height of the sand dune at 1 min. is higher than that for non-porous one. There was almost no change for more than 5 min. after the beginning of the test. The sand movements are extremely intensive just behind the fence as well as the top of the dune. As previously described, the process of sand-dune erosion depends on the conditions of the installed fence. In Figure 9, the shapes of the eroded surface with different porosity fences are compared. Although a sedimentation area was found close behind the non-porous fence, the sand bed around - 7 -

8 Fig. 12 Stream lines of instantaneous flow field around a fence: (a) non-porous fence, (b) ε = 1%, (c) ε = 3%, (d) ε = 5%. the porous fence was found to be more eroded as the porosity rate was increased. However, the height of the remaining sand dune at 1 min. was high as the porosity rate was increased. It can be supposed that these characteristic shapes of dune surface were influenced by the air flow around the dune. These shapes of dune surface were different each other. These different features depended on whether the fence had porosity or not. According to the distribution of U and U rms, these features are schematically depicted in Fig.1, which presents a diagram of the deformed dune surface. In this figure, the black solid and dot lines show the initial dune surface and the eroded one, respectively. It seems that the flow condition along the dune surface should affect the sand movements. A significant erosion can be observed at the surface far downstream from the fence, where a highspeed air flow induces sand movements because its velocity is higher than a critical friction velocity. Moreover, another strongly eroded surface can be found below the region (shaded area in the figure), where a high turbulent intensity makes the critical friction velocity small. In such a case, sand particles moved away even in the low-velocity air flow. For instance, the area just behind a porous fence was eroded remarkably under the low magnitude of U. As can be seen in Fig. 1, the dune erosion is apparently influenced by whether or not a fence has the porosity. The flow field around the fence and its dependency on the porosity rate will be discussed in the following section. Flow Field around Fence on Flat Plane T he flow field around a fence on a flat plane was measured using PIV. Here, four porosity rates (ε = %, 1%, 3%, 5%) for the fence were tested. Figure 11 shows the time-averaged flow fields. The horizontal axis (x) is the streamwise distance in the measurement area, and the vertical axis (y) is the wall-normal distance normalized by the height of the fence. The contour shows the distribution of the streamwise turbulent intensity U rms. The solid lines with vectors indicate the streamlines. In the case of the non-porous fence, the separated flow from the fence edge has large values of U rms and it continually grows out of the measurement area. The separated flow became weak and small as the porosity rate was increased. In contrast, the value of U rms just behind fence is large, especially - 8 -

9 velocity.4.2 U * U *ct /(d p g) 1/2 velocity x/h f.4.2 U * U *ct /(d p g) 1/ x/h f x/h f (a) (b) (c) (d) velocity U * U *ct /(d p g) 1/2 velocity.4.2 U * U *ct /(d p g) 1/ x/h f Fig. 13 Relationship between critical friction velocity and streamwise velocity along bottom surface: (a) non-porous fence, (b) ε = 1%, (c) ε = 3%, (d) ε = 5%. for ε = 3% and 5%. This is attributed to a grid turbulence, i.e., separated flows from apertures of the porous fence. Although the turbulent intensity became large with increasing the porosity rate, an area downstream of the high turbulent intensity region was calm comparatively. In Fig. 11(a), a reverse flow existed just behind the fence, which was induced by the separated flow. Okamoto et al. (26) performed a LDV measurement on the flow field around a fence and their obtained distribution of streamlines is consistent with our result. A secondary vortex just behind the foot of the fence is also found in Fig. 11(a). This small vortex is induced by the reverse flow. For the case of the porous fence, the wall-normal velocity around the fence edge became small as the porosity rate was increased. This tendency represents the fluid upstream of the fence through the porous fence. The reverse flow behind the non-porous fence contracted with increasing the porosity, and it finally disappeared. Figure 12 shows the instantaneous velocity field in the same region with that of Fig. 11. The number of streamlines from the left side of the measurement area is same in each case. For the case of the non-porous fence, the density of stream lines was high above the fence, implying the velocity was high there. As the porosity was increased, the velocity gradient became small. Hence, some large-scale eddies were found to occur in the downstream of the porous fence. When the 1% or 3% porous fence was installed, the vortices just behind the fence were few, and the reverse flow behind the fence became small. In the case of the 5% porosity fence, there was no reverse-flow region. Therefore, the flow behind the fence seemed to be rectified by the porous fence. The difference between the flow with a non-porous fence and that with a porous one is obviously significant. It seems that the shape of sand dune surface was influenced by these flow fields around the fence. Critical Friction Velocity Behind Fence In this section, we discuss a relation between the sand movement and the velocity along the dune surface. As mentioned in the introduction, a threshold of the air-flow velocity about sand movements was firstly introduced by Bagnold (1956), and it is called a critical friction velocity. His definition does not consider the influence of the velocity fluctuation on the critical friction velocity. Shimazu et al. (28) had carried out experiments, in which the diameter of test sand grains, the moisture contained in the sand bed, and the turbulence statistics of air flows were measured, and had clarified their effects on the critical friction velocity. In general, the sand particle starts to move under the flow condition of the higher velocity than the critical friction velocity. They clarified that, when the magnitude of the wall-normal velocity fluctuation increased, the sand particles were moved by lower air-flow velocity because of the decreased critical friction velocity. According to their work, the critical friction velocity U *ct is determined as following for particles - 9 -

10 larger than 1 µm, d * ' ct p u v' = 2 p g H d p g d p 4. Conclusion U Fc β. (1) d g τ w The value of β is The capillary force Fc is assumed to be constant in this study. In Fig. 13, the critical friction velocity, which is obtained from Eq. (1), and the measured velocity at 1.6 mm height above are compared the flat plane. The horizontal axis is the distance from the fence along the flat plane. In an area where U > U *ct, sand particles move away. For the cases of the non-porous and the 1%-porosity fence, U *ct is larger than U throughout this measurement area. Hence the sand movement hardly occurred. When the 3%-porosity fence was installed, there exists an area where sand movement occurs because of U > U *ct. In the case of the 5%-porosity fence, a difference of these two velocities is much larger than that for the 3% case, so that the mass flux of sand movement is large. These results are in consistent with the shape of dune surface just behind the fence (see, for instance, Fig. 9). The dune surface just behind the non-porous fence gave rise to a sedimentation area. In the case of the 1%-porosity fence, the dune surface behind the fence was eroded, but there remained the tendency of the sedimentation. For 3% and 5% porosity, the intensive erosion area just behind the fence corresponds to the area where U > U *ct. According to these results, the relation between the flow field and the shape of dune surface around the fence can be explained with the Eq. (1) qualitatively. These results conform to the tendency of the eroded sand dune surface. The erosion of dune surface just behind fence became intensive as the fence porosity became large. We investigated the effect of a porous fence, which was installed on an upstream surface of a model dune, on the dune erosion and the relationship between the erosion and flow field around the dune. The process of erosion was measured by the visualization using a laser sheet. The flow field around the dune and the fence on flat plane were measured by LDV and PIV systems, respectively. It is found that the porous fence was effective to depress the separated flow from the edge of the fence. However, the decelerated air flow through the porous fence had high turbulent intensity just behind fence. Hence, there was intensive erosion area just behind fence, while at the top of the dune the erosion was avoided. This tendency is more remarkable as the porosity is increased. The flow field around a fence was different in each porosity rate. We confirmed that the empirical correlation of the critical friction velocity, proposed by Shimazu et al. (28), can be applied to sand movements influenced by a fence. 5. References B. Andreotti, P. Claudin, and S. Douady. Selection of dune shapes and velocities Part 1: Dynamics of sand, wind and barchans. European Physical Journal B, 28: , 22a. B. Andreotti, P. Claudin, and S. Douady. Selection of dune shapes and velocities Part 2: A twodimensional modeling. European Physical Journal B, 28: , 22b. R. A. Bagnold. The Physics of blown sand and desert dunes. Dover publications, Inc., H. G. Kim and V. C. Patel, Test of turbulence models for wind flow over terrain with separation and recirculation. Boundary-Layer Meteorology, 94: 5-21,

11 S. J. Lee and H. B. Kim. Velocity field measurements of flow around a triangular prism behind a porous fence. Journal of Wind Engineering and Industrial Aerodynamics, 77-78: , S. J. Lee and H. C. Lim. A numerical study on flow around a triangular prism located behind a porous fence. Fluid Dynamics Research, 28: , 21. S. J. Lee, K. C. Park, and C. W. Park, Wind tunnel observations about the shelter effect of porous fences on the sand particle movements. Atmospheric Environment, 36: , 22. X. R. Li, X. P. Wang, T. Li, J. G. Zhang, Microbiotic soil crust and its effect on vegetation and habitat on artificially stabilized desert dunes in Tengger Desert, North China. Biol Fertil Soils, 35: , 22 S. Okamoto, A. Shimane, N. Kubota, Flow around Two Perforated Plates Placed Perpendicularly on a Ground Plane, Transactions of the Japan Society of Mechanical Engineers. B 72:717: ,26. T. Sakamoto, Y. Ishida, and H. Hagino, Wind tunnel study on the effect of a wind break fence constructed on an embankment. Journal of the Japan Society of Erosion Control Engineering, 58: 49-53, 25. Y. Sakamoto, S. Shimazu, T. Tsukahara, M. Yamamoto and Y. Kawaguchi. Control of sand movement on model dune by fence installation experimental study using LDV. Turbulence, Heat and Mass transfer, 6 (eds. K. Hanjalić et al.), Begell House Inc., 91-94, 29. S. Shimazu, M. Sakai, T, Kimura, M. Yamamoto and Y. Kawaguchi. Experimental investigation of the critical friction velocity for sand movement from the fixed source in the air flow: effect of the critical friction velocity on a turbulence phenomenon. In Proc. of 7th JSME- KSME Thermal and Fluid Engineering Conference, Oct , Sapporo, Japan, K142, (CD-ROM) 4 pp., 28 I. J. Walker, W. G. Nickling, Simulation and measurement of surface shear stress over isolated and closely spaced transverse dunes in a wind tunnel. Earth Surf. Process. Landforms 28: ,

SIMULTANEOUS VELOCITY AND CONCENTRATION MEASUREMENTS OF A TURBULENT JET MIXING FLOW

SIMULTANEOUS VELOCITY AND CONCENTRATION MEASUREMENTS OF A TURBULENT JET MIXING FLOW Proceedings of International Symposium on Visualization and Image in Transport Phenomena, Turkey, -9 Oct. SIMULTANEOUS VELOCITY AND CONCENTRATION MEASUREMENTS OF A TURBULENT JET MIXING FLOW Hui HU a, Tetsuo

More information

Simultaneous Velocity and Concentration Measurements of a Turbulent Jet Mixing Flow

Simultaneous Velocity and Concentration Measurements of a Turbulent Jet Mixing Flow Simultaneous Velocity and Concentration Measurements of a Turbulent Jet Mixing Flow HUI HU, a TETSUO SAGA, b TOSHIO KOBAYASHI, b AND NOBUYUKI TANIGUCHI b a Department of Mechanical Engineering, Michigan

More information

THE EFFECT OF SAMPLE SIZE, TURBULENCE INTENSITY AND THE VELOCITY FIELD ON THE EXPERIMENTAL ACCURACY OF ENSEMBLE AVERAGED PIV MEASUREMENTS

THE EFFECT OF SAMPLE SIZE, TURBULENCE INTENSITY AND THE VELOCITY FIELD ON THE EXPERIMENTAL ACCURACY OF ENSEMBLE AVERAGED PIV MEASUREMENTS 4th International Symposium on Particle Image Velocimetry Göttingen, Germany, September 7-9, 00 PIV 0 Paper 096 THE EFFECT OF SAMPLE SIZE, TURBULECE ITESITY AD THE VELOCITY FIELD O THE EXPERIMETAL ACCURACY

More information

Colloquium FLUID DYNAMICS 2013 Institute of Thermomechanics AS CR, v.v.i., Prague, October 23-25, 2013 p.1

Colloquium FLUID DYNAMICS 2013 Institute of Thermomechanics AS CR, v.v.i., Prague, October 23-25, 2013 p.1 Colloquium FLUID DYNAMICS 2013 Institute of Thermomechanics AS CR, v.v.i., Prague, October 23-25, 2013 p.1 ON THE REYNOLDS NUMBER ROLE IN STRUCTURE OF RECIRCULATION ZONE BEHIND BACKWARD FACING STEP IN

More information

The Seventh International Colloquium on Bluff Body Aerodynamics and Applications (BBAA7) Shanghai, China; September 2-6, 2012 Study on characteristics

The Seventh International Colloquium on Bluff Body Aerodynamics and Applications (BBAA7) Shanghai, China; September 2-6, 2012 Study on characteristics Study on characteristics of ore storage-pile fugitive-dust based on wind tunnel experiments Yonghua Xue a a Tianjin Research Institute for Water Transport Engineering of Ministry of Transport, 2618#, Xingang

More information

Wind tunnel test on the effect of metal net fences on sand flux in a Gobi Desert, China

Wind tunnel test on the effect of metal net fences on sand flux in a Gobi Desert, China J Arid Land (2017) 9(6): 888 899 https://doi.org/10.1007/s40333-017-0068-5 Science Press Springer-Verlag Wind tunnel test on the effect of metal net fences on sand flux in a Gobi Desert, China WANG Tao

More information

Experimental investigation of flow control devices for the reduction of transonic buffeting on rocket afterbodies

Experimental investigation of flow control devices for the reduction of transonic buffeting on rocket afterbodies Experimental investigation of flow control devices for the reduction of transonic buffeting on rocket afterbodies F.F.J. Schrijer 1, A. Sciacchitano 1, F. Scarano 1 1: Faculty of Aerospace Engineering,

More information

Flow Characteristics around an Inclined Circular Cylinder with Fin

Flow Characteristics around an Inclined Circular Cylinder with Fin Lisbon, Portugal, 7- July, 28 Flow Characteristics around an Inclined Circular Cylinder with Fin Tsuneaki ISHIMA, Takeshi SASAKI 2, Yoshitsugu GOKAN 3 Yasushi TAKAHASHI 4, Tomio OBOKATA 5 : Department

More information

Dual Vortex Structure Shedding from Low Aspect Ratio, Surface-mounted Pyramids

Dual Vortex Structure Shedding from Low Aspect Ratio, Surface-mounted Pyramids Dual Vortex Structure Shedding from Low Aspect Ratio, Surface-mounted Pyramids Robert J. Martinuzzi Department of Mechanical and Manufacturing Engineering Schulich School of Engineering University of Calgary

More information

DYNAMICS OF CONTROLLED BOUNDARY LAYER SEPARATION

DYNAMICS OF CONTROLLED BOUNDARY LAYER SEPARATION p.1 DYNAMICS OF CONTROLLED BOUNDARY LAYER SEPARATION Václav Uruba, Martin Knob Institute of Thermomechanics, AS CR, v. v. i., Praha Abstract: The results of experimental study on a boundary layer separation

More information

Active drag reduction in a turbulent boundary layer based on plasma-actuatorgenerated streamwise vortices

Active drag reduction in a turbulent boundary layer based on plasma-actuatorgenerated streamwise vortices June 30 - July 3, 015 Melbourne, Australia 9 9A-5 Active drag reduction in a turbulent boundary layer based on plasma-actuatorgenerated streamwise vortices Chi Wai Wong, Yu Zhou, Yinzhe Li and Yupeng Li

More information

elements remain in high frequency region and sometimes very large spike-shaped peaks appear. So we corrected the PIV time histories by peak cutting an

elements remain in high frequency region and sometimes very large spike-shaped peaks appear. So we corrected the PIV time histories by peak cutting an The Seventh International Colloquium on Bluff Body Aerodynamics and Applications (BBAA7) Shanghai, China; September 2-6, 2012 LES of fluctuating wind pressure on a 3D square cylinder for PIV-based inflow

More information

On the influence of bed permeability on flow in the leeside of coarse-grained bedforms

On the influence of bed permeability on flow in the leeside of coarse-grained bedforms On the influence of bed permeability on flow in the leeside of coarse-grained bedforms G. Blois (1), J. L. Best (1), G. H. Sambrook Smith (2), R. J. Hardy (3) 1 University of Illinois, Urbana-Champaign,

More information

Experimental characterization of flow field around a square prism with a small triangular prism

Experimental characterization of flow field around a square prism with a small triangular prism Journal of Mechanical Science and Technology 29 (4) (2015) 1649~1656 www.springerlink.com/content/1738-494x OI 10.1007/s12206-015-0336-2 Experimental characterization of flow field around a square prism

More information

y * x * Shumpei HARA

y * x * Shumpei HARA th International Symposium on Turbulence and Shear Flow Phenomena (TSFP), Chicago, USA, July, 7 ANALYSIS OF THE TURBULENT KINETIC ENERGY BUDGET FOR MEANDERING MOTION APPEARING IN A BACKWARD-FACING STEP

More information

Aqueous and Aeolian Bedforms

Aqueous and Aeolian Bedforms Aqueous and Aeolian Bedforms 1 Further reading & review articles R.A. Bagnold, 1941, The physics of blown sand and desert dunes Charru et al., 2013, Sand ripples and dunes, Ann. Review of Fluid Mech. 2

More information

FLOW VISUALIZATION AND PIV MEASUREMENTS OF LAMINAR SEPARATION BUBBLE OSCILLATING AT LOW FREQUENCY ON AN AIRFOIL NEAR STALL

FLOW VISUALIZATION AND PIV MEASUREMENTS OF LAMINAR SEPARATION BUBBLE OSCILLATING AT LOW FREQUENCY ON AN AIRFOIL NEAR STALL 4 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES FLOW VISUALIZATION AND PIV MEASUREMENTS OF LAMINAR SEPARATION BUBBLE OSCILLATING AT LOW FREQUENCY ON AN AIRFOIL NEAR STALL Hiroyuki Tanaka Department

More information

A PIV study of flow over interacting Barchan dunes

A PIV study of flow over interacting Barchan dunes A PIV study of flow over interacting Barchan dunes Jessica A. Palmer 1, Ricardo Mejia-Alvarez 2, Eric M. Rivera 3, James L. Best 4 and Kenneth T. Christensen 5 1: Department of Geology, University of Illinois,

More information

Visualization of wall turbulence under artificial disturbance by piezo actuator array

Visualization of wall turbulence under artificial disturbance by piezo actuator array Visualization of wall turbulence under artificial disturbance by piezo actuator array By Takehiko Segawa *, Peiwen Li **, Yasuo Kawaguchi * and Hiro Yoshida * *Mechanical Engineering Laboratory, AIST MITI,

More information

Density Field Measurement by Digital Laser Speckle Photography

Density Field Measurement by Digital Laser Speckle Photography Density Field Measurement by Digital Laser Speckle Photography by M. Kawahashi and H. Hirahara Saitama University Department of Mechanical Engineering Shimo-Okubo 255, Urawa, Saitama, 338-8570, Japan ABSTRACT

More information

Sand transport over a barchan dune

Sand transport over a barchan dune Sand transport over a barchan dune F. Charru (1), V. Laval (1) 1. IMFT, Toulouse, France - corresponding author: francois.charru@imft.fr Abstract The present work investigates an important and yet unsolved

More information

Flow Control around Bluff Bodies by Attached Permeable Plates

Flow Control around Bluff Bodies by Attached Permeable Plates Flow Control around Bluff Bodies by Attached Permeable Plates G. M. Ozkan, H. Akilli Abstract The aim of present study is to control the unsteady flow structure downstream of a circular cylinder by use

More information

Dynamics of Large Scale Motions in Bubble-Driven Turbulent Flow

Dynamics of Large Scale Motions in Bubble-Driven Turbulent Flow Dynamics of Large Scale Motions in Bubble-Driven Turbulent Flow Kyung Chun Kim School of Mechanical Engineering, Pusan National University Jangjeon-dong, Geumjeong-gu, Pusan, 609-735, Korea kckim@pusan.ac.kr

More information

PASSIVE CONTROL ON JET MIXING FLOWS BY USING VORTEX GENERATORS

PASSIVE CONTROL ON JET MIXING FLOWS BY USING VORTEX GENERATORS Proceedings of the Sixth Triennial International Symposium on Fluid Control, Measurement and Visualization, Sherbrooke, Canada, August -7,. PASSIVE CONTROL ON JET MIXING FLOWS BY USING VORTEX GENERATORS

More information

Journal of Fluid Science and Technology

Journal of Fluid Science and Technology Science and Technology LDV and PIV Measurements of the Organized Oscillations of Turbulent Flow over a Rectangular Cavity* Takayuki MORI ** and Kenji NAGANUMA ** **Naval Systems Research Center, TRDI/Ministry

More information

HORSEHOE VORTICES IN UNIFORMLY SHEARED TURBULENCE

HORSEHOE VORTICES IN UNIFORMLY SHEARED TURBULENCE HORSEHOE VORTICES IN UNIFORMLY SHEARED TURBULENCE Christina Vanderwel Department of Mechanical Engineering University of Ottawa Ottawa, Ontario, Canada cvand072@uottawa.ca Stavros Tavoularis Department

More information

White Paper FINAL REPORT AN EVALUATION OF THE HYDRODYNAMICS MECHANISMS WHICH DRIVE THE PERFORMANCE OF THE WESTFALL STATIC MIXER.

White Paper FINAL REPORT AN EVALUATION OF THE HYDRODYNAMICS MECHANISMS WHICH DRIVE THE PERFORMANCE OF THE WESTFALL STATIC MIXER. White Paper FINAL REPORT AN EVALUATION OF THE HYDRODYNAMICS MECHANISMS WHICH DRIVE THE PERFORMANCE OF THE WESTFALL STATIC MIXER Prepared by: Dr. Thomas J. Gieseke NUWCDIVNPT - Code 8233 March 29, 1999

More information

25 years of PIV development for application in aeronautical test facilities

25 years of PIV development for application in aeronautical test facilities 25 years of PIV development for application in aeronautical test facilities Jürgen Kompenhans and team Department Experimental Methods Institute of Aerodynamics and Flow Technology German Aerospace Center

More information

Turbulence Laboratory

Turbulence Laboratory Objective: CE 319F Elementary Mechanics of Fluids Department of Civil, Architectural and Environmental Engineering The University of Texas at Austin Turbulence Laboratory The objective of this laboratory

More information

Vortex shedding from slender surface mounted pyramids

Vortex shedding from slender surface mounted pyramids Vortex shedding from slender surface mounted pyramids M. J. Morrison 1, R. J. Martinuzzi 3, E. Savory 1, G. A. Kopp 2 1 Department of Mechanical and Materials Engineering, University of Western Ontario,

More information

Fluid Flow Characteristics of a Swirl Jet Impinging on a Flat Plate

Fluid Flow Characteristics of a Swirl Jet Impinging on a Flat Plate Fluid Flow Characteristics of a Swirl Jet Impinging on a Flat Plate Juliana K. Abrantes 1, Luis Fernando A. Azevedo 2 1: Department of Mechanical Engineering, PUC-Rio, Rio de Janeiro, Brazil, kuhlmann@mec.puc-rio.br

More information

Observations of Giant Bursts Associated with Microscale Breaking Waves

Observations of Giant Bursts Associated with Microscale Breaking Waves Observations of Giant Bursts Associated with Microscale Breaking Waves Ira Leifer and Sanjoy Banerjee a) Chemical Engineering Department, University of California, Santa Barbara, Santa Barbara, California,

More information

Symmetry of Turbulent Characteristics Inside Urban Intersection

Symmetry of Turbulent Characteristics Inside Urban Intersection Colloquium FLUID DYNAMICS 2007 Institute of Thermomechanics AS CR, v. v. i., Prague, October 24-26, 2007 p.1 Symmetry of Turbulent Characteristics Inside Urban Intersection Radka Kellnerová 1,2 Zbyněk

More information

Flow measurements over a moving sandy bed

Flow measurements over a moving sandy bed Flow measurements over a moving sandy bed by Costa, MAV; Teixeira, SFCF and Teixeira, JCF School of Engineering University of Minho 48-58 Guimarães, Portugal ABSTRACT In understanding the behaviour of

More information

Convection in Three-Dimensional Separated and Attached Flow

Convection in Three-Dimensional Separated and Attached Flow Convection in Three-Dimensional Separated and Attached Flow B. F. Armaly Convection Heat Transfer Laboratory Department of Mechanical and Aerospace Engineering, and Engineering Mechanics University of

More information

PROPERTIES OF THE FLOW AROUND TWO ROTATING CIRCULAR CYLINDERS IN SIDE-BY-SIDE ARRANGEMENT WITH DIFFERENT ROTATION TYPES

PROPERTIES OF THE FLOW AROUND TWO ROTATING CIRCULAR CYLINDERS IN SIDE-BY-SIDE ARRANGEMENT WITH DIFFERENT ROTATION TYPES THERMAL SCIENCE, Year, Vol. 8, No. 5, pp. 87-9 87 PROPERTIES OF THE FLOW AROUND TWO ROTATING CIRCULAR CYLINDERS IN SIDE-BY-SIDE ARRANGEMENT WITH DIFFERENT ROTATION TYPES by Cheng-Xu TU, a,b Fu-Bin BAO

More information

Experimental Study of Near Wake Flow Behind a Rectangular Cylinder

Experimental Study of Near Wake Flow Behind a Rectangular Cylinder American Journal of Applied Sciences 5 (8): 97-926, 28 ISSN 546-9239 28 Science Publications Experimental Study of Near Wake Flow Behind a Rectangular Cylinder Abdollah Shadaram, Mahdi Azimi Fard and Noorallah

More information

Transformation of barchans into parabolic dunes under the influence of vegetation

Transformation of barchans into parabolic dunes under the influence of vegetation Transformation of barchans into parabolic dunes under the influence of vegetation arxiv:cond-mat/0504621 v1 25 Apr 2005 Abstract O. Durán, V. Schatz, H. J. Herrmann Institute for Computer Physics, Universität

More information

PIV STUDY OF LONGITUDINAL VORTICES IN A TURBULENT BOUNDARY LAYER FLOW

PIV STUDY OF LONGITUDINAL VORTICES IN A TURBULENT BOUNDARY LAYER FLOW ICAS CONGRESS PIV STUDY OF LONGITUDINAL VORTICES IN A TURBULENT BOUNDARY LAYER FLOW G. M. Di Cicca Department of Aerospace Engineering, Politecnico di Torino C.so Duca degli Abruzzi, 4 - I 19 Torino, ITALY

More information

Paper ID ICLASS EFFECTS OF CAVITATION IN A NOZZLE ON LIQUID JET ATOMIZATION

Paper ID ICLASS EFFECTS OF CAVITATION IN A NOZZLE ON LIQUID JET ATOMIZATION ICLASS- Aug.7-Sept.1,, Kyoto, Japan Paper ID ICLASS-3 EFFECTS OF CAVITATION IN A NOZZLE ON LIQUID JET ATOMIZATION Akira Sou 1, Maulana Muhaad Ilham, Shigeo Hosokawa 3 and Akio Tomiyama 1 Assistant Professor,

More information

Investigation of Transonic Flow Behavior around a Three- Dimensional Turret Using Particle Image Velocimetry

Investigation of Transonic Flow Behavior around a Three- Dimensional Turret Using Particle Image Velocimetry Investigation of Transonic Flow Behavior around a Three- Dimensional Turret Using Particle Image Velocimetry Carlos Caballero College of Engineering, University of Florida Light distortions produced by

More information

Journal of Fluid Science and Technology

Journal of Fluid Science and Technology Bulletin of the JSME Vol.9, No.3, 24 Journal of Fluid Science and Technology Re-evaluating wake width in turbulent shear flow behind an axisymmetric cylinder by means of higher order turbulence statistics

More information

HEAT TRANSFER AND FLOW CHARACTERISTICS OF A BACKWARD-FACING STEP FLOW WITH MIST

HEAT TRANSFER AND FLOW CHARACTERISTICS OF A BACKWARD-FACING STEP FLOW WITH MIST Paper No. IMPRES13-119 HEAT TRANSFER AND FLOW CHARACTERISTICS OF A BACKWARD-FACING STEP FLOW WITH MIST Masaki HIGA 1,*, Izuru SENAHA, Yoshitaka MIYAFUJI 3, Sumio KATO and Shoichi MATSUDA 1 Graduate School

More information

EXPERIMENTAL INVESTIGATION OF THREE DIMENSIONAL SEPARATED FLOW OVER A BODY OF REVOLUTION AT HIGH ANGLES OF ATTACK

EXPERIMENTAL INVESTIGATION OF THREE DIMENSIONAL SEPARATED FLOW OVER A BODY OF REVOLUTION AT HIGH ANGLES OF ATTACK ICAS CONGRESS EXPERIMENTAL INVESTIGATION OF THREE DIMENSIONAL SEPARATED FLOW OVER A BODY OF Tadateru Ishide 1), Nobuhide Nishikawa ) and Fumihiko Mikami ) 1)Kisarazu National College of Technology, -11-1,kiyomidai-higashi,

More information

PDA Measurements of Single Point Injection in Cross-flow

PDA Measurements of Single Point Injection in Cross-flow PDA Measurements of Single Point Injection in Cross-flow by M.J. Melo, J.M.M. Sousa and M. Costa Instituto Superior Técnico, Mechanical Engineering Department Av. Rovisco Pais, 1049-001 Lisboa, Portugal

More information

Figure 1. Schematic of experimental setup.

Figure 1. Schematic of experimental setup. June 3 - July 3, Melbourne, Australia 9 9D- STRUCTURE OF 3D OFFSET JETS OVER A SURFACE MOUNTED SQUARE RIB Shawn P. Clark Department of Civil Engineering 7A Chancellors Circle, Winnipeg, Manitoba, R3T V,

More information

PARTICLE MOTION IN WATER-PARTICLE, GAS-PARTICLE AND GAS-DROPLET TWO-PHASE FLOWS

PARTICLE MOTION IN WATER-PARTICLE, GAS-PARTICLE AND GAS-DROPLET TWO-PHASE FLOWS ISTP-6, 5, PRAGUE 6 TH INTERNATIONAL SYMPOSIUM ON TRANSPORT PHENOMENA PARTICLE MOTION IN WATER-PARTICLE, GAS-PARTICLE AND GAS-DROPLET TWO-PHASE FLOWS Tsuneaki ISHIMA*, Masaaki YOKOTA**, Toshimichi ARAI***,

More information

This is an author-deposited version published in : Eprints ID : 10568

This is an author-deposited version published in :  Eprints ID : 10568 Open Archive TOULOUSE Archive Ouverte (OATAO) OATAO is an open access repository that collects the work of Toulouse researchers and makes it freely available over the web where possible. This is an author-deposited

More information

PIV measurements and convective heat transfer of an impinging air jet

PIV measurements and convective heat transfer of an impinging air jet PIV measurements and convective heat transfer of an impinging air jet by T. S. O Donovan (), D. B. Murray () and A.A. Torrance (3) Department of Mechanical & Manufacturing Engineering, Trinity College

More information

Effect of blowing rate on the film cooling coverage on a multi-holed plate: application on combustor walls

Effect of blowing rate on the film cooling coverage on a multi-holed plate: application on combustor walls Effect of blowing rate on the film cooling coverage on a multi-holed plate: application on combustor walls P. Miron 1,2, C. Berat 1 & V. Sabelnikov 3 1 TURBOMECA-Bordes, France 2 LaTEP, Université de Pau

More information

2/23/2009. Visualizing Earth Science. Chapter Overview. Deserts and Drylands. Glaciers and Ice Sheets

2/23/2009. Visualizing Earth Science. Chapter Overview. Deserts and Drylands. Glaciers and Ice Sheets Visualizing Earth Science By Z. Merali and B. F. Skinner Chapter 6 Deserts, Glaciers and Ice Sheets Chapter Overview Deserts and Drylands Glaciers and Ice Sheets Deserts Geography Categorization of deserts

More information

Flow disturbance due to presence of the vane anemometer

Flow disturbance due to presence of the vane anemometer Journal of Physics: Conference Series OPEN ACCESS Flow disturbance due to presence of the vane anemometer To cite this article: M Bujalski et al 24 J. Phys.: Conf. Ser. 53 245 View the article online for

More information

Experiments on the perturbation of a channel flow by a triangular ripple

Experiments on the perturbation of a channel flow by a triangular ripple Experiments on the perturbation of a channel flow by a triangular ripple F. Cúñez *, E. Franklin Faculty of Mechanical Engineering, University of Campinas, Brazil * Correspondent author: fernandodcb@fem.unicamp.br

More information

Turbulence is a ubiquitous phenomenon in environmental fluid mechanics that dramatically affects flow structure and mixing.

Turbulence is a ubiquitous phenomenon in environmental fluid mechanics that dramatically affects flow structure and mixing. Turbulence is a ubiquitous phenomenon in environmental fluid mechanics that dramatically affects flow structure and mixing. Thus, it is very important to form both a conceptual understanding and a quantitative

More information

Percolation: Statistical Description of a Spatial and Temporal Highly Resolved Boundary Layer Transition

Percolation: Statistical Description of a Spatial and Temporal Highly Resolved Boundary Layer Transition Percolation: Statistical Description of a Spatial and Temporal Highly Resolved Boundary Layer Transition Tom T. B. Wester, Dominik Traphan, Gerd Gülker and Joachim Peinke Abstract In this article spatio-temporally

More information

Chapter 5 Phenomena of laminar-turbulent boundary layer transition (including free shear layers)

Chapter 5 Phenomena of laminar-turbulent boundary layer transition (including free shear layers) Chapter 5 Phenomena of laminar-turbulent boundary layer transition (including free shear layers) T-S Leu May. 3, 2018 Chapter 5: Phenomena of laminar-turbulent boundary layer transition (including free

More information

Flow Structure Investigations in a "Tornado" Combustor

Flow Structure Investigations in a Tornado Combustor Flow Structure Investigations in a "Tornado" Combustor Igor Matveev Applied Plasma Technologies, Falls Church, Virginia, 46 Serhiy Serbin National University of Shipbuilding, Mikolayiv, Ukraine, 545 Thomas

More information

Open Access Experimental Research and Analysis of Vortex Excited Vibration Suppression of Spiral Stripe Strake

Open Access Experimental Research and Analysis of Vortex Excited Vibration Suppression of Spiral Stripe Strake Send Orders for Reprints to reprints@benthamscience.ae The Open Mechanical Engineering Journal, 2014, 8, 941-947 941 Open Access Experimental Research and Analysis of Vortex Excited Vibration Suppression

More information

ANALYSIS OF TURBULENT FLOW IN THE IMPELLER OF A CHEMICAL PUMP

ANALYSIS OF TURBULENT FLOW IN THE IMPELLER OF A CHEMICAL PUMP Journal of Engineering Science and Technology Vol. 2, No. 3 (2007) 218-225 School of Engineering, Taylor s University College ANALYSIS OF TURBULENT FLOW IN THE IMPELLER OF A CHEMICAL PUMP MIN-GUAN YANG,

More information

Transactions on Engineering Sciences vol 9, 1996 WIT Press, ISSN

Transactions on Engineering Sciences vol 9, 1996 WIT Press,   ISSN A study of turbulence characteristics in open channel transitions as a function of Froude and Reynolds numbers using Laser technique M.I.A. El-shewey, S.G. Joshi Department of Civil Engineering, Indian

More information

Turbulence characteristics of flow in an open channel with temporally varying mobile bedforms

Turbulence characteristics of flow in an open channel with temporally varying mobile bedforms J. Hydrol. Hydromech., 65, 2017, 1, 35 48 DOI: 10.1515/johh-2016-0044 Turbulence characteristics of flow in an open channel with temporally varying mobile bedforms Prashanth Reddy Hanmaiahgari 1*, Vesselina

More information

Large-Eddy Simulation for Turbulent Nature of Flow and Pressure Fields over Urban Building Arrays C. Hirose*, A. Hagishima, N. Ikegaya, and J. Tanimot

Large-Eddy Simulation for Turbulent Nature of Flow and Pressure Fields over Urban Building Arrays C. Hirose*, A. Hagishima, N. Ikegaya, and J. Tanimot Large-Eddy Simulation for Turbulent Nature of Flow and Pressure Fields over Urban Building Arrays C. Hirose*, A. Hagishima, N. Ikegaya, and J. Tanimoto Interdisciplinary Graduate School of Engineering

More information

Information on the Particle Dynamics Analysis (PDA) measurements

Information on the Particle Dynamics Analysis (PDA) measurements Information on the Particle Dynamics Analysis (PDA) measurements Contents Contents... Introduction... Properties of the PDA System... Measurement principles []... Information on the variables in each column

More information

Flow over ripples: KEY features ripple size independent of flow depth l ~ 1000d deceleration in leeside topographic acceleration over stoss flow

Flow over ripples: KEY features ripple size independent of flow depth l ~ 1000d deceleration in leeside topographic acceleration over stoss flow Ripples and dunes Flow over ripples: KEY features ripple size independent of flow depth l ~ 1000d deceleration in leeside topographic acceleration over stoss flow separation in leeside shear layer development

More information

Experimental Investigation of the Aerodynamic Forces and Pressures on Dome Roofs: Reynolds Number Effects

Experimental Investigation of the Aerodynamic Forces and Pressures on Dome Roofs: Reynolds Number Effects Experimental Investigation of the Aerodynamic Forces and Pressures on Dome Roofs: Reynolds Number Effects *Ying Sun 1), Ning Su 2), Yue Wu 3) and Qiu Jin 4) 1), 2), 3), 4) Key Lab of Structures Dynamic

More information

Design and Aerodynamic Characterization of a Synthetic Jet for Boundary Layer Control

Design and Aerodynamic Characterization of a Synthetic Jet for Boundary Layer Control Design and Aerodynamic Characterization of a Synthetic Jet for Boundary Layer Control FRANCESCA SATTA, DANIELE SIMONI, MARINA UBALDI, PIETRO ZUNINO Department of Fluid Machines, Energy Systems, and Transportation

More information

PARTICLE IMAGE VELOCIMETRY AND PROPER ORTHOGONAL DECOMPOSITION ANALYSIS OF THE CHANNEL FLOW EQUIPPED WITH CYLINDRICAL RIBS.

PARTICLE IMAGE VELOCIMETRY AND PROPER ORTHOGONAL DECOMPOSITION ANALYSIS OF THE CHANNEL FLOW EQUIPPED WITH CYLINDRICAL RIBS. PARTICLE IMAGE VELOCIMETRY AND PROPER ORTHOGONAL DECOMPOSITION ANALYSIS OF THE CHANNEL FLOW EQUIPPED WITH CYLINDRICAL RIBS Cahit Gurlek Department of Mechanical Engineering, University of Cumhuriyet, 58140

More information

Evolution of the pdf of a high Schmidt number passive scalar in a plane wake

Evolution of the pdf of a high Schmidt number passive scalar in a plane wake Evolution of the pdf of a high Schmidt number passive scalar in a plane wake ABSTRACT H. Rehab, L. Djenidi and R. A. Antonia Department of Mechanical Engineering University of Newcastle, N.S.W. 2308 Australia

More information

NUMERICAL APPROACH TO INTER-FIBER FLOW IN NON-WOVENS WITH SUPER ABSORBENT FIBERS

NUMERICAL APPROACH TO INTER-FIBER FLOW IN NON-WOVENS WITH SUPER ABSORBENT FIBERS THERMAL SCIENCE, Year 2017, Vol. 21, No. 4, pp. 1639-1644 1639 Introduction NUMERICAL APPROACH TO INTER-FIBER FLOW IN NON-WOVENS WITH SUPER ABSORBENT FIBERS by Zhi-Rong DING a*, Ying GUO a b, and Shan-Yuan

More information

Aerodynamic characteristics of two-dimensional sharp-edged objects in tandem arrangement )

Aerodynamic characteristics of two-dimensional sharp-edged objects in tandem arrangement ) Arch. Mech., 60, 6, pp. 475 490, Warszawa 2008 SIXTY YEARS OF THE ARCHIVES OF MECHANICS Aerodynamic characteristics of two-dimensional sharp-edged objects in tandem arrangement ) R. GNATOWSKA Institute

More information

7. Basics of Turbulent Flow Figure 1.

7. Basics of Turbulent Flow Figure 1. 1 7. Basics of Turbulent Flow Whether a flow is laminar or turbulent depends of the relative importance of fluid friction (viscosity) and flow inertia. The ratio of inertial to viscous forces is the Reynolds

More information

International Journal of Scientific & Engineering Research, Volume 6, Issue 5, May ISSN

International Journal of Scientific & Engineering Research, Volume 6, Issue 5, May ISSN International Journal of Scientific & Engineering Research, Volume 6, Issue 5, May-2015 28 CFD BASED HEAT TRANSFER ANALYSIS OF SOLAR AIR HEATER DUCT PROVIDED WITH ARTIFICIAL ROUGHNESS Vivek Rao, Dr. Ajay

More information

Visualization of high-speed gas jets and their airblast sprays of cross-injected liquid

Visualization of high-speed gas jets and their airblast sprays of cross-injected liquid Short communications Experiments in Fluids 27 (1999) 102 106 Springer-Verlag 1999 Visualization of high-speed gas jets and their airblast sprays of cross-injected liquid K. D. Kihm, T. K. Kim, S. Y. Son

More information

Fluid Mechanics. Chapter 9 Surface Resistance. Dr. Amer Khalil Ababneh

Fluid Mechanics. Chapter 9 Surface Resistance. Dr. Amer Khalil Ababneh Fluid Mechanics Chapter 9 Surface Resistance Dr. Amer Khalil Ababneh Wind tunnel used for testing flow over models. Introduction Resistances exerted by surfaces are a result of viscous stresses which create

More information

PIV-INVESTIGATIONS OF INTERNAL SLIT NOZZLE FLOWS AND THEIR INFLUENCE ON LIQUID SHEET BREAKUP

PIV-INVESTIGATIONS OF INTERNAL SLIT NOZZLE FLOWS AND THEIR INFLUENCE ON LIQUID SHEET BREAKUP ILASS-Europe 2002 Zaragoza 9 11 September 2002 PIV-INVESTIGATIONS OF INTERNAL SLIT NOZZLE FLOWS AND THEIR INFLUENCE ON LIQUID SHEET BREAKUP J. Scholz, K. Roetmann, V. Beushausen Jochen.Scholz@llg.gwdg.de

More information

PIV study for the analysis of planar jets in cross-flow at low Reynolds number

PIV study for the analysis of planar jets in cross-flow at low Reynolds number PIV study for the analysis of planar jets in cross-flow at low Reynolds number Vincenti I., Guj G., Camussi R., Giulietti E. University Roma TRE, Department of Ingegneria Meccanica e Industriale (DIMI),

More information

A Comparative Study of the PIV and LDV Measurements on a Self-induced Sloshing Flow

A Comparative Study of the PIV and LDV Measurements on a Self-induced Sloshing Flow 2000 The Visualization Society of Japan and Ohmsha, Ltd. Journal of Visualization, Vol. 3, No.2 (2000) 145-156 A Comparative Study of the PIV and LDV Measurements on a Self-induced Sloshing Flow Saga,

More information

PIV Applications to Thermal Performance of LPG

PIV Applications to Thermal Performance of LPG PIV Applications to Thermal Performance of LPG Cooking Burner BY USA MAKMOOL And PROF.SUMRERNG JUGJAI Assoc. PROF. SUVIT TIA 1. Rational/ Problem Statement LPG consumption of Household sector (Thailand,

More information

Electrostatic Precipitator Utilizing Gradient-force

Electrostatic Precipitator Utilizing Gradient-force Proc. ESA Annual Meeting on Electrostatics 2013 1 Electrostatic Precipitator Utilizing Gradient-force Atsushi Katatani Department of Business Development & Promotion Panasonic Environmental Systems & Engineering

More information

Investigation of the flow in a flat bottom cyclone

Investigation of the flow in a flat bottom cyclone Investigation of the flow in a flat bottom cyclone by B. Chiné (1) and F. Concha (2) (1) Catholic University of Concepción, Faculty of Engineering Campus San Andrés, Paicavi 000, Concepción, Chile E-mail:

More information

Calculation of the separation streamlines of barchans and transverse dunes

Calculation of the separation streamlines of barchans and transverse dunes Calculation of the separation streamlines of barchans and transverse dunes H. J. Herrmann a,b, J. S. Andrade Jr. b, V. Schatz a, G. Sauermann a and E. J. R. Parteli a a ICP, University of Stuttgart, Pfaffenwaldring

More information

AN UNSTEADY AND TIME-AVERAGED STUDY OF A GROUND VORTEX FLOW

AN UNSTEADY AND TIME-AVERAGED STUDY OF A GROUND VORTEX FLOW 24 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES AN UNSTEADY AND TIME-AVERAGED STUDY OF A GROUND VORTEX FLOW N J Lawson*, J M Eyles**, K Knowles** *College of Aeronautics, Cranfield University,

More information

PIV Measurements of turbulence statistics and near-wall structure of fully developed pipe flow at high Reynolds number

PIV Measurements of turbulence statistics and near-wall structure of fully developed pipe flow at high Reynolds number 6th International Symposium on Particle Image Velocimetry Pasadena, California, USA, September 21-23, 2005 PIV 05 Paper nnnn PIV Measurements of turbulence statistics and near-wall structure of fully developed

More information

THE INFLUENCE OF NICKS ON THE SOUND PROPERTIES AND THE AIRFLOW IN FRONT OF FLUE ORGAN PIPE

THE INFLUENCE OF NICKS ON THE SOUND PROPERTIES AND THE AIRFLOW IN FRONT OF FLUE ORGAN PIPE THE INFLUENCE OF NICKS ON THE SOUND PROPERTIES AND THE AIRFLOW IN FRONT OF FLUE ORGAN PIPE Zdeněk Otčenášek, Viktor Hruška, Ondřej Moravec, Martin Švejda Musical Acoustics Research Centre Academy of Performing

More information

Chuichi Arakawa Graduate School of Interdisciplinary Information Studies, the University of Tokyo. Chuichi Arakawa

Chuichi Arakawa Graduate School of Interdisciplinary Information Studies, the University of Tokyo. Chuichi Arakawa Direct Numerical Simulations of Fundamental Turbulent Flows with the Largest Grid Numbers in the World and its Application of Modeling for Engineering Turbulent Flows Project Representative Chuichi Arakawa

More information

Growing and decaying processes and resistance of sand waves in the vicinity of the Tone River mouth

Growing and decaying processes and resistance of sand waves in the vicinity of the Tone River mouth Advances in River Sediment Research Fukuoka et al. (eds) 2013 Taylor & Francis Group, London, ISBN 978-1-138-00062-9 Growing and decaying processes and resistance of sand waves in the vicinity of the Tone

More information

The Fluid Flow in the T-Junction. The Comparison of the Numerical Modeling and Piv Measurement

The Fluid Flow in the T-Junction. The Comparison of the Numerical Modeling and Piv Measurement Available online at www.sciencedirect.com Procedia Engineering 39 (2012 ) 19 27 XIIIth International Scientific and Engineering Conference HERVICON-2011 The Fluid Flow in the T-Junction. The Comparison

More information

Correlations between turbulent wall pressure and velocity field fluctuations in backward-facing step

Correlations between turbulent wall pressure and velocity field fluctuations in backward-facing step DocumentID: 450038 Correlations between turbulent wall pressure and velocity field fluctuations in backward-facing step flows Istvan Bolgar, Sven Scharnowski, and Christian J. Kähler Bundeswehr University

More information

TURBULENCE IN MICRO-CHANNELS

TURBULENCE IN MICRO-CHANNELS ExHFT-7 28 June 03 July 2009, Krakow, Poland TURBULENCE IN MICRO-CHANNELS T. A. Kowalewski *, S. Blonski IPPT PAN, Polish Academy of Sciences, Warsaw, Poland ABSTRACT. Fluid mechanics in small channels,

More information

arxiv: v1 [physics.flu-dyn] 27 Aug 2016

arxiv: v1 [physics.flu-dyn] 27 Aug 2016 Morphology and displacement of dunes in a closed-conduit flow, arxiv:1608.07729v1 [physics.flu-dyn] 27 Aug 2016 E.M. Franklin, F. Charru Institut de Mécanique des Fluides de Toulouse, Allée du Pr. Camille

More information

Module 3: Velocity Measurement Lecture 16: Validation of PIV with HWA. The Lecture Contains: Hotwire Anemometry. Uncertainity

Module 3: Velocity Measurement Lecture 16: Validation of PIV with HWA. The Lecture Contains: Hotwire Anemometry. Uncertainity The Lecture Contains: Hotwire Anemometry Hotwire Measurements Calibration Methodology Curve Fitting Directional Probe Senstivity Data Reduction Uncertainity Validation of Experiments Comparision of Hot

More information

Large-eddy simulation of flow over barchan dunes

Large-eddy simulation of flow over barchan dunes Large-eddy simulation of flow over barchan dunes M. Omidyeganeh (1), U. Piomelli (1), K. T. Christensen (2), and J. L. Best (2) 1. Queen s University, Kingston, CA omidyeganeh@me.queensu.ca, ugo@me.queensu.ca

More information

17th International Conference on Harmonisation within Atmospheric Dispersion Modelling for Regulatory Purposes 9-12 May 2016, Budapest, Hungary

17th International Conference on Harmonisation within Atmospheric Dispersion Modelling for Regulatory Purposes 9-12 May 2016, Budapest, Hungary 17th International Conference on Harmonisation within Atmospheric Dispersion Modelling for Regulatory Purposes 9-12 May 2016, Budapest, Hungary INVESTIGATION OF VENTILATION AND AIR QUALITY IN URBAN SQUARES

More information

Comparison between Numerical and Experimental for UVP Measurement in Double Bent Pipe with Out-of-Plane Angle

Comparison between Numerical and Experimental for UVP Measurement in Double Bent Pipe with Out-of-Plane Angle Journal of Flow Control, Measurement & Visualization, 24, 2, 54-64 Published Online October 24 in SciRes. http://www.scirp.org/journal/jfcmv http://dx.doi.org/.4236/jfcmv.24.247 Comparison between Numerical

More information

18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics LISBON PORTUGAL JULY 4 7, 2016.

18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics LISBON PORTUGAL JULY 4 7, 2016. Multiple-eye PIV Eisaku Atsumi 1, Jun Sakakibara 2,* 1: Graduate School of Science and Technology, Meji university 2: Department of Mechanical Engineering, Meji university * Correspondent author: sakakiba@meiji.ac.jp

More information

GENERALISATION OF THE TWO-SCALE MOMENTUM THEORY FOR COUPLED WIND TURBINE/FARM OPTIMISATION

GENERALISATION OF THE TWO-SCALE MOMENTUM THEORY FOR COUPLED WIND TURBINE/FARM OPTIMISATION 25 th National Symposium on Wind Engineering, Tokyo, Japan, 3-5 December 2018 第 25 回風工学シンポジウム (2018) GENERALISATION OF THE TWO-SCALE MOMENTUM THEORY FOR COUPLED WIND TURBINE/FARM OPTIMISATION Takafumi

More information

RESEARCH ON THE SELF-INDUCED SLOSHING PHENOMENA IN A RECTANGULAR TANK

RESEARCH ON THE SELF-INDUCED SLOSHING PHENOMENA IN A RECTANGULAR TANK 9TH. INTERNATIONAL SYMPOSIUM ON FLOW VISUALIZATION, RESEARCH ON THE SELF-INDUCED SLOSHING PHENOMENA IN A RECTANGULAR TANK Tetsuo SAGA, Hui HU, Toshio KOBAYASHI Shigeki SEGAWA and Nobuyuki TANIGUCHI Keywords:

More information

Internal Flow Measurements of Turbomachinery using PIV

Internal Flow Measurements of Turbomachinery using PIV Internal Flow Measurements of Turbomachinery using PIV OHUCHIDA Satoshi : Turbo Machinery and Engine Technology Department, Products Development Center, Corporate Research & Development TAMAKI Hideaki

More information

Effect of bed form evolution on sediment erosion and suspended load transport in an impinging jet

Effect of bed form evolution on sediment erosion and suspended load transport in an impinging jet th 17 International Symposium on Applications of Laser Techniques to Fluid Mechanics Effect of bed form evolution on sediment erosion and suspended load transport in an impinging jet Ken T Kiger1,*, Kyle

More information

NPTEL Quiz Hydraulics

NPTEL Quiz Hydraulics Introduction NPTEL Quiz Hydraulics 1. An ideal fluid is a. One which obeys Newton s law of viscosity b. Frictionless and incompressible c. Very viscous d. Frictionless and compressible 2. The unit of kinematic

More information