Research Interests:
- Experimental fluid dynamics
- Bluff body and vehicle aerodynamics
- Model reduction techniques such as POD, DMD, or FMD (Fourier Mode Decomposition)
- Vortex-induced-vibration
- PIV and time-resolved PIV
- Cavitation
- Nucleation effects on cavitation
- Microbubble generation and measurement
Publications:
2017 |
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![]() | Venning, James A; Lo Jacono, David ; Burton, David; Thompson, Mark C; Sheridan, John The nature of the vortical structures in the near wake of the Ahmed body Journal Article Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering, 231 (9), pp. 1239–1244, 2017, ISSN: 09544070. @article{Venning2017, title = {The nature of the vortical structures in the near wake of the Ahmed body}, author = {James A Venning and David {Lo Jacono} and David Burton and Mark C Thompson and John Sheridan}, url = {https://jamesvenning.net/wp-content/uploads/2015/11/Venning-et-al.-2017-The-nature-of-the-vortical-structures-in-the-near-wake-of-the-Ahmed-body.pdf}, doi = {10.1177/0954407017690683}, issn = {09544070}, year = {2017}, date = {2017-01-01}, journal = {Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering}, volume = {231}, number = {9}, pages = {1239--1244}, abstract = {This study presents the results from high-spatial-resolution water-channel velocity-field measurements behind an Ahmed body with 25° rear slant angle. The Ahmed body represents a simplified generic model of a hatchback automobile that has been widely used to study near-wake flow dynamics. The results help clarify the unresolved question of whether the time-mean near-wake flow structure is topologically equivalent to a toroidal vortex or better described by a pair of horizontally aligned horseshoe vortices, with their legs pointing downstream. The velocimetry data presented allows the tracking of the vortical structures throughout the near wake through a set of orthogonal planes, as well as the measurement of their circulation. The spanwise vortices that form as the flow separates from the top and bottom rear edges are shown to tilt downstream at the sides of the body, while no evidence is found of a time-mean attached toroidal vortex, at least for the Reynolds number (based on the square root of the frontal area) of R e FA ∼ 30, 000 under consideration.}, keywords = {}, pubstate = {published}, tppubtype = {article} } This study presents the results from high-spatial-resolution water-channel velocity-field measurements behind an Ahmed body with 25° rear slant angle. The Ahmed body represents a simplified generic model of a hatchback automobile that has been widely used to study near-wake flow dynamics. The results help clarify the unresolved question of whether the time-mean near-wake flow structure is topologically equivalent to a toroidal vortex or better described by a pair of horizontally aligned horseshoe vortices, with their legs pointing downstream. The velocimetry data presented allows the tracking of the vortical structures throughout the near wake through a set of orthogonal planes, as well as the measurement of their circulation. The spanwise vortices that form as the flow separates from the top and bottom rear edges are shown to tilt downstream at the sides of the body, while no evidence is found of a time-mean attached toroidal vortex, at least for the Reynolds number (based on the square root of the frontal area) of R e FA ∼ 30, 000 under consideration. |
Khoo, M T; Venning, J A; Takahashi, K; Arai, J; Mori, T; Pearce, B W; Brandner, P A Joint Research between Australia and Japan on the Cavitation Inception of Marine Propellers and Control Surfaces Inproceedings MAST Asia Conference, 2017. @inproceedings{Khoo2017, title = {Joint Research between Australia and Japan on the Cavitation Inception of Marine Propellers and Control Surfaces}, author = {M T Khoo and J A Venning and K Takahashi and J Arai and T Mori and B W Pearce and P A Brandner}, year = {2017}, date = {2017-01-01}, booktitle = {MAST Asia Conference}, abstract = {International defence research collaboration between regional allies fosters the symbiotic development of scientific expertise and enables benchmarking of techniques and results. On 1 December 2015, Australia's Minister of Defence and Japan's Min- ister of Defense signed a Letter of Arrangement concerning joint research on Marine Hydrodynamics. This four-year research program is the first defence science and technology collaboration between Australia's Defence Science and Technology Group (DST) and Japan's Acquisition, Technology & Logistics Agency (ATLA). In this project, ATLA's Flow Noise Simulator and the cavitation tunnel at the Australian Maritime College (AMC), an institute of the University of Tasmania with which DST has partnered, are being used to conduct hydrodynamic testing to develop ex- pertise and experience with regard to cavitation inception about propellers and control surfaces of marine platforms. The phenomenon of cavitation occurs when a fluid changes from its liquid to vapour phase due to pressure reduction. This can be detrimental to the hydrodynamic, acoustic and structural performance of marine platforms. The complimentary features of the Australian and Japanese test facilities are described in this paper and sample results from joint measurements of cavitation nuclei size distributions in the respective cavitation tunnels are presented. The implications of the results and the future work program are also discussed.}, keywords = {}, pubstate = {published}, tppubtype = {inproceedings} } International defence research collaboration between regional allies fosters the symbiotic development of scientific expertise and enables benchmarking of techniques and results. On 1 December 2015, Australia's Minister of Defence and Japan's Min- ister of Defense signed a Letter of Arrangement concerning joint research on Marine Hydrodynamics. This four-year research program is the first defence science and technology collaboration between Australia's Defence Science and Technology Group (DST) and Japan's Acquisition, Technology & Logistics Agency (ATLA). In this project, ATLA's Flow Noise Simulator and the cavitation tunnel at the Australian Maritime College (AMC), an institute of the University of Tasmania with which DST has partnered, are being used to conduct hydrodynamic testing to develop ex- pertise and experience with regard to cavitation inception about propellers and control surfaces of marine platforms. The phenomenon of cavitation occurs when a fluid changes from its liquid to vapour phase due to pressure reduction. This can be detrimental to the hydrodynamic, acoustic and structural performance of marine platforms. The complimentary features of the Australian and Japanese test facilities are described in this paper and sample results from joint measurements of cavitation nuclei size distributions in the respective cavitation tunnels are presented. The implications of the results and the future work program are also discussed. | |
![]() | Smith, Samuel; Venning, James; Giosio, Dean; Brandner, Paul; Pearce, Bryce; Young, Yin Lu Cloud cavitation behaviour on a hydrofoil due to fluid-structure interaction Inproceedings Open Archives of the 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2017, 2017. @inproceedings{Smith2017, title = {Cloud cavitation behaviour on a hydrofoil due to fluid-structure interaction}, author = {Samuel Smith and James Venning and Dean Giosio and Paul Brandner and Bryce Pearce and Yin Lu Young}, url = {https://jamesvenning.net/wp-content/uploads/2020/06/2017-ISROMAC-smith-etal.pdf}, year = {2017}, date = {2017-01-01}, booktitle = {Open Archives of the 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2017}, abstract = {Despite recent extensive research into fluid-structure interaction (FSI) of cavitating hydrofoils there remains insufficient experimental data to explain many of these observed phenomena. The cloud cavitation behaviour around a hydrofoil due to the effect of FSI is investigated utilizing rigid and compliant 3D hydrofoils held in a cantilevered configuration in a cavitation tunnel. The hydrofoils have identical undeformed geometry of tapered planform with constant NACA0009 section. The rigid model is made of stainless steel and the compliant model of carbon and glass fibre reinforced epoxy resin with the structural fibres aligned along the span-wise direction to avoid material bend-twist coupling. Tests were conducted at an incidence of 6°, a mean chord based Reynolds number of 0.7 × 106, and cavitation number of 0.8. Force measurements were simultaneously acquired with high-speed imaging to enable correlation of forces with tip bending deformations and cavity physics. Hydrofoil compliance was seen to dampen the higher frequency force fluctuations while showing strong correlation between normal force and tip deflection. The 3D nature of the flow field was seen to cause complex cavitation behaviour with two shedding modes observed on both models.}, keywords = {}, pubstate = {published}, tppubtype = {inproceedings} } Despite recent extensive research into fluid-structure interaction (FSI) of cavitating hydrofoils there remains insufficient experimental data to explain many of these observed phenomena. The cloud cavitation behaviour around a hydrofoil due to the effect of FSI is investigated utilizing rigid and compliant 3D hydrofoils held in a cantilevered configuration in a cavitation tunnel. The hydrofoils have identical undeformed geometry of tapered planform with constant NACA0009 section. The rigid model is made of stainless steel and the compliant model of carbon and glass fibre reinforced epoxy resin with the structural fibres aligned along the span-wise direction to avoid material bend-twist coupling. Tests were conducted at an incidence of 6°, a mean chord based Reynolds number of 0.7 × 106, and cavitation number of 0.8. Force measurements were simultaneously acquired with high-speed imaging to enable correlation of forces with tip bending deformations and cavity physics. Hydrofoil compliance was seen to dampen the higher frequency force fluctuations while showing strong correlation between normal force and tip deflection. The 3D nature of the flow field was seen to cause complex cavitation behaviour with two shedding modes observed on both models. |
![]() | Venning, James; Smith, Samuel; Brandner, Paul; Giosio, Dean; Pearce, Bryce The influence of nuclei content on cloud cavitation about a hydrofoil Inproceedings Open Archives of the 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2017, pp. 2–7, 2017. @inproceedings{Venning2017b, title = {The influence of nuclei content on cloud cavitation about a hydrofoil}, author = {James Venning and Samuel Smith and Paul Brandner and Dean Giosio and Bryce Pearce}, url = {https://jamesvenning.net/wp-content/uploads/2020/06/2017-ISROMAC-venning-etal.pdf}, year = {2017}, date = {2017-01-01}, booktitle = {Open Archives of the 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2017}, volume = {2}, pages = {2--7}, abstract = {The dynamics of cloud cavitation about a 3D hydrofoil are investigated experimentally in a cavitation tunnel with both an abundance and dearth of freestream nuclei. The rectangular-planform, NACA 0015 hydrofoil was tested at a Reynolds number of 1.4 × 106, a cavitation number of 0.55 and an incidence of 6°. High-speed photography of cavitation shedding phenomena was acquired simultaneously with unsteady force measurement to enable identification of cavity shedding modes corresponding with force spectral peaks. Two shedding modes are evident for both the nuclei deplete and abundant cases, although each are driven by different flow phenomena. The high-frequency mode for the nuclei deplete case is driven primarily by large-scale re-entrant jet formation during the growth phase, but shockwave propagation for the collapse phase of the cycle. The weaker low-frequency mode occurs because the strength of shedding at the hydrofoil tip varies at half the fundamental frequency. The dominant mode for the abundant case is the low-frequency mode which is some 1.8 times slower than the nuclei deplete case. The high-frequency mode for the nuclei abundant case is due to the propagation of two shockwaves; the passage of the first only partially condenses the cavity, while the second condenses a much larger region of the cavity.}, keywords = {}, pubstate = {published}, tppubtype = {inproceedings} } The dynamics of cloud cavitation about a 3D hydrofoil are investigated experimentally in a cavitation tunnel with both an abundance and dearth of freestream nuclei. The rectangular-planform, NACA 0015 hydrofoil was tested at a Reynolds number of 1.4 × 106, a cavitation number of 0.55 and an incidence of 6°. High-speed photography of cavitation shedding phenomena was acquired simultaneously with unsteady force measurement to enable identification of cavity shedding modes corresponding with force spectral peaks. Two shedding modes are evident for both the nuclei deplete and abundant cases, although each are driven by different flow phenomena. The high-frequency mode for the nuclei deplete case is driven primarily by large-scale re-entrant jet formation during the growth phase, but shockwave propagation for the collapse phase of the cycle. The weaker low-frequency mode occurs because the strength of shedding at the hydrofoil tip varies at half the fundamental frequency. The dominant mode for the abundant case is the low-frequency mode which is some 1.8 times slower than the nuclei deplete case. The high-frequency mode for the nuclei abundant case is due to the propagation of two shockwaves; the passage of the first only partially condenses the cavity, while the second condenses a much larger region of the cavity. |
2016 |
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![]() | Venning, J Vortex structures in the wakes of two- and three-dimensional bodies PhD Thesis Monash University, 2016. @phdthesis{Venning2016PhD, title = {Vortex structures in the wakes of two- and three-dimensional bodies}, author = {J Venning}, url = {https://jamesvenning.net/wp-content/uploads/2020/04/Venning-2016-Vortex-structures-in-the-wakes-of-two-and-three-dimensional-bodies.pdf}, year = {2016}, date = {2016-01-01}, school = {Monash University}, abstract = {This thesis reports on an experimental study into the flow structure of two different bluff bodies: an inclined flat plate with a quasi-two-dimensional wake and the Ahmed body with a highly three-dimensional wake. Each wake is measured using particle image velocimetry with high spatial and temporal resolution. Time-average results are presented showing the effect of angle-of-attack and Reynolds number on the flow around the flat plate. Results showing the formation of large scale von Kármán vortices from the merging of smaller shear layer vortices is presented and the ratio of these frequencies is quantified. The nature of the major wake structures of the Ahmed body is presented and the strength of each structure is quantified through measuring the circulation. An analysis of the circulation variation with downstream location reveals the tilting of vorticity and the subsequent merging of structures. The dynamics of the vortex motion is illustrated using two-dimensional space-time plots revealing large, periodic motions in the wake. The influence of the longitudinal structures on the wake is investigated by systematically varying the lateral spacing of the c-pillars. By increasing the rear-slant aspect ratio, the induced downwash between the two longitudinal structures is reduced. The critical aspect ratio between reattaching and completely separated flow is presented. The effect of aspect ratio on the dynamics of these structures is shown to be minimal.}, keywords = {}, pubstate = {published}, tppubtype = {phdthesis} } This thesis reports on an experimental study into the flow structure of two different bluff bodies: an inclined flat plate with a quasi-two-dimensional wake and the Ahmed body with a highly three-dimensional wake. Each wake is measured using particle image velocimetry with high spatial and temporal resolution. Time-average results are presented showing the effect of angle-of-attack and Reynolds number on the flow around the flat plate. Results showing the formation of large scale von Kármán vortices from the merging of smaller shear layer vortices is presented and the ratio of these frequencies is quantified. The nature of the major wake structures of the Ahmed body is presented and the strength of each structure is quantified through measuring the circulation. An analysis of the circulation variation with downstream location reveals the tilting of vorticity and the subsequent merging of structures. The dynamics of the vortex motion is illustrated using two-dimensional space-time plots revealing large, periodic motions in the wake. The influence of the longitudinal structures on the wake is investigated by systematically varying the lateral spacing of the c-pillars. By increasing the rear-slant aspect ratio, the induced downwash between the two longitudinal structures is reduced. The critical aspect ratio between reattaching and completely separated flow is presented. The effect of aspect ratio on the dynamics of these structures is shown to be minimal. |
![]() | Russell, P S; Giosio, D R; Venning, J A; Pearce, B W; Brandner, P A Microbubble Generation from Condensation and Turbulent Breakup of Sheet Cavitation Inproceedings 31st Symposium on Naval Hydrodynamics, Monterery, 2016. @inproceedings{Russell2016, title = {Microbubble Generation from Condensation and Turbulent Breakup of Sheet Cavitation}, author = {P S Russell and D R Giosio and J A Venning and B W Pearce and P A Brandner}, url = {https://jamesvenning.net/wp-content/uploads/2015/11/Russell-et-al.-2016-Microbubble-Generation-from-Condensation-and-Turbulent-Breakup-of-Sheet-Cavitation.pdf}, year = {2016}, date = {2016-01-01}, booktitle = {31st Symposium on Naval Hydrodynamics}, address = {Monterery}, abstract = {The formation, size and concentration of microbub- bles generated in the wake of a cavitating hydrofoil are investigated experimentally for several Reynolds and cavitation numbers. The presentwork is restricted to bubble generation from stable sheet cavitation. Interactions between the cavity, the overlying boundary layer and associated interfacial effects are investigated qualitatively and quantitatively using high-resolution and high-speed photography. The physics of cavity breakup and conden- sation and microbubble formation are also investigated using high-speed photography. Size and concentration of microbubble populations are measured in the far wake using diffused laser shadowgraphy. The optical setup of the shadowgraphy permitted microbubbles in the size range of 5 to 300 µm to be resolved. Coherent spatial and temporal features of the sheet cavitation are shown to be functions of both Reynolds and cavitation numbers. For the range of microbubble sizes measured, concentrations are shown to increase with Reynolds number and reduce with decreasing cavitation number. In contrast, void fraction increases with decreasing cavitation number indicating a greater production of larger diameter bubbles.}, keywords = {}, pubstate = {published}, tppubtype = {inproceedings} } The formation, size and concentration of microbub- bles generated in the wake of a cavitating hydrofoil are investigated experimentally for several Reynolds and cavitation numbers. The presentwork is restricted to bubble generation from stable sheet cavitation. Interactions between the cavity, the overlying boundary layer and associated interfacial effects are investigated qualitatively and quantitatively using high-resolution and high-speed photography. The physics of cavity breakup and conden- sation and microbubble formation are also investigated using high-speed photography. Size and concentration of microbubble populations are measured in the far wake using diffused laser shadowgraphy. The optical setup of the shadowgraphy permitted microbubbles in the size range of 5 to 300 µm to be resolved. Coherent spatial and temporal features of the sheet cavitation are shown to be functions of both Reynolds and cavitation numbers. For the range of microbubble sizes measured, concentrations are shown to increase with Reynolds number and reduce with decreasing cavitation number. In contrast, void fraction increases with decreasing cavitation number indicating a greater production of larger diameter bubbles. |
![]() | Khoo, M T; Venning, J A; Pearce, B W; Brandner, P A; Lecoffre, Y Development of a Cavitation Susceptibility Meter for Nuclei Size Distribution Measurements Inproceedings 20th Australasian Fluid Mechanics Conference, 2016. @inproceedings{Khoo2016, title = {Development of a Cavitation Susceptibility Meter for Nuclei Size Distribution Measurements}, author = {M T Khoo and J A Venning and B W Pearce and P A Brandner and Y Lecoffre}, url = {https://jamesvenning.net/wp-content/uploads/2015/11/Khoo-et-al.-2016-Development-of-a-Cavitation-Susceptibility-Meter-for-Nuclei-Size-Distribution-Measurements.pdf}, year = {2016}, date = {2016-01-01}, booktitle = {20th Australasian Fluid Mechanics Conference}, abstract = {Cavitation inception in practical flows is invariably heterogeneous as nucleation sites are provided by microbubble populations. Microbubbles grow explosively, filling with vapour, when exposed to a critical pressure which is size dependent. The detection of physical bubble activations in a known pressure field can therefore be used to measure bubble size distributions. The nuclei population within a test flow can be measured using a venturi and by counting the number of activations or events using the acoustic emission from each bubble collapse in the downstream pressure recovery region. Such devices are known as Cavitation Susceptibility Meters (CSMs). The development, calibration and operation of a CSM for use in the cavitation tunnel at the Australian Maritime College is described. The minimum pressure in the CSM is reduced in steps by increasing the flow rate or decreasing tunnel static pressure to activate increasing numbers of smaller nuclei in order to provide a cumulative size distribution. Simultaneous flow rate measurement permits nuclei volumetric concentration as well as venturi throat pressure to be determined. The concentration measurement is shown to have an uncertainty of less than 0.5%, while the critical pressure has an uncertainty of approximately 5%. The volume measurement and timing uncertainties for flow rate calibration are found to account for 81% of this uncertainty. Sample nuclei distribution measurements are presented, showing critical pressures as low as 100 kPa below vapour pressure, corresponding to an equivalent bubble diameter of 1 µm in the test section.}, keywords = {}, pubstate = {published}, tppubtype = {inproceedings} } Cavitation inception in practical flows is invariably heterogeneous as nucleation sites are provided by microbubble populations. Microbubbles grow explosively, filling with vapour, when exposed to a critical pressure which is size dependent. The detection of physical bubble activations in a known pressure field can therefore be used to measure bubble size distributions. The nuclei population within a test flow can be measured using a venturi and by counting the number of activations or events using the acoustic emission from each bubble collapse in the downstream pressure recovery region. Such devices are known as Cavitation Susceptibility Meters (CSMs). The development, calibration and operation of a CSM for use in the cavitation tunnel at the Australian Maritime College is described. The minimum pressure in the CSM is reduced in steps by increasing the flow rate or decreasing tunnel static pressure to activate increasing numbers of smaller nuclei in order to provide a cumulative size distribution. Simultaneous flow rate measurement permits nuclei volumetric concentration as well as venturi throat pressure to be determined. The concentration measurement is shown to have an uncertainty of less than 0.5%, while the critical pressure has an uncertainty of approximately 5%. The volume measurement and timing uncertainties for flow rate calibration are found to account for 81% of this uncertainty. Sample nuclei distribution measurements are presented, showing critical pressures as low as 100 kPa below vapour pressure, corresponding to an equivalent bubble diameter of 1 µm in the test section. |
![]() | Crouch, T N N; Burton, D; Venning, J A A; Thompson, M C C; Brown, N A T A T; Sheridan, J A comparison of the wake structures of scale and full-scale pedalling cycling models Journal Article Procedia Engineering, 147 , pp. 13–19, 2016, ISSN: 1877-7058. @article{Crouch2016, title = {A comparison of the wake structures of scale and full-scale pedalling cycling models}, author = {T N N Crouch and D Burton and J A A Venning and M C C Thompson and N A T A T Brown and J Sheridan}, url = {https://jamesvenning.net/wp-content/uploads/2020/04/1-s2.0-S1877705816306294-main.pdf}, doi = {10.1016/j.proeng.2016.06.182}, issn = {1877-7058}, year = {2016}, date = {2016-01-01}, journal = {Procedia Engineering}, volume = {147}, pages = {13--19}, publisher = {The Author(s)}, abstract = {This paper presents a novel approach to better understand the unsteady aerodynamics associated with a dynamically pedalling cyclist. Using high resolution Particle Image Velocimetry (PIV) in a water channel, the large-scale wake structure is analysed for various phases of the crank cycle of a 1:4.5 scale-model cyclist/bicycle under both static and pedalling conditions. Both quasi-steady and dynamic pedalling leg results are compared with detailed velocity field surveys made in the wake of a full-scale pedalling cyclist mannequin of similar geometry and position in a wind tunnel. A time-averaged and phase-averaged analysis of the various flow regimes that occur throughout the pedal stroke shows good agreement between scale-model and full-scale mannequin investigations. This highlights the robustness of the formation of the primary wake flow structures when subjected to varying Reynolds number, bicycle/rider geometry and quasi-steady/dynamic pedalling conditions.}, keywords = {}, pubstate = {published}, tppubtype = {article} } This paper presents a novel approach to better understand the unsteady aerodynamics associated with a dynamically pedalling cyclist. Using high resolution Particle Image Velocimetry (PIV) in a water channel, the large-scale wake structure is analysed for various phases of the crank cycle of a 1:4.5 scale-model cyclist/bicycle under both static and pedalling conditions. Both quasi-steady and dynamic pedalling leg results are compared with detailed velocity field surveys made in the wake of a full-scale pedalling cyclist mannequin of similar geometry and position in a wind tunnel. A time-averaged and phase-averaged analysis of the various flow regimes that occur throughout the pedal stroke shows good agreement between scale-model and full-scale mannequin investigations. This highlights the robustness of the formation of the primary wake flow structures when subjected to varying Reynolds number, bicycle/rider geometry and quasi-steady/dynamic pedalling conditions. |
![]() | Venning, J A; Vincentis, De S; Pearce, B W; Brandner, P A Microbubble generation for PIV seeding. Inproceedings 20th Australasian Fluid Mechanics Conference, Perth, 2016. @inproceedings{Venning2016a, title = {Microbubble generation for PIV seeding.}, author = {J A Venning and De S Vincentis and B W Pearce and P A Brandner}, url = {https://jamesvenning.net/wp-content/uploads/2016/11/microbubbles.pdf}, year = {2016}, date = {2016-01-01}, booktitle = {20th Australasian Fluid Mechanics Conference}, number = {December}, address = {Perth}, abstract = {A new device for microbubble generation using small-scale unsteady cavitation of supersaturated water is presented. Cavitation is created in a radial diffuser with a directed outlet for inlet/saturation pressures ranging from 300 to 1000 kPa. The diffuser is formed using an acrylic plate spaced 50 µm above a 0.5 mm diameter outlet. Optical access is provided via the acrylic plate enabling investigation of the basic flow properties of the cavitation and microbubble trajectories using PIV. The size distribution and production rate of the generated microbubbles are measured using diffused-laser shadowgraphy and longranging microscopy within the emerging liquid jet. The size distribution of the microbubble population is suitable for PIV, with all bubbles produced being less than 25 µm. Microbubble production rates in excess of 100 million bubbles per second are achievable. The variation of the generated microbubble population for various operating conditions is presented}, keywords = {}, pubstate = {published}, tppubtype = {inproceedings} } A new device for microbubble generation using small-scale unsteady cavitation of supersaturated water is presented. Cavitation is created in a radial diffuser with a directed outlet for inlet/saturation pressures ranging from 300 to 1000 kPa. The diffuser is formed using an acrylic plate spaced 50 µm above a 0.5 mm diameter outlet. Optical access is provided via the acrylic plate enabling investigation of the basic flow properties of the cavitation and microbubble trajectories using PIV. The size distribution and production rate of the generated microbubbles are measured using diffused-laser shadowgraphy and longranging microscopy within the emerging liquid jet. The size distribution of the microbubble population is suitable for PIV, with all bubbles produced being less than 25 µm. Microbubble production rates in excess of 100 million bubbles per second are achievable. The variation of the generated microbubble population for various operating conditions is presented |
2015 |
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![]() | Crouch, T N; Barry, N; Venning, J A; Burton, D; Thompson, M C; Sheridan, J The application of laser diagnostics to cycling aerodynamics Inproceedings 7th Australian Conference on Laser Diagnostics in Fluid Mechanics and Combustion, pp. 161–165, 2015. @inproceedings{Crouch2015, title = {The application of laser diagnostics to cycling aerodynamics}, author = {T N Crouch and N Barry and J A Venning and D Burton and M C Thompson and J Sheridan}, url = {https://jamesvenning.net/wp-content/uploads/2015/11/ACLDFMC7_Cyclist.pdf}, year = {2015}, date = {2015-01-01}, booktitle = {7th Australian Conference on Laser Diagnostics in Fluid Mechanics and Combustion}, number = {December}, pages = {161--165}, abstract = {To improve the aerodynamic performance of cyclists, detailed information of the flow field is required around these highly three-dimensional bluff-body geometries. Using traditional measurement techniques with cyclists in a wind tunnel, it is often difficult or impractical to acquire detailed flow field surveys. In this paper two examples are discussed where highresolution Particle Image Velocimetry has been undertaken in a water channel to investigate the wake dynamics of a single pedalling cyclist and the flow between multiple cyclists. These areas have previously been difficult to measure experimentally using intrusive measurement techniques. The first example provides a comparison of the phase-averaged wake of a 1:4.5 scale pedalling cyclist/bicycle combination in the water channel and that of a full-scale cyclist mannequin of similar geometry and position in a wind tunnel. The second example shows an application of PIV to measure the flow field between two drafting cyclists. Good agreement is observed between the large-scale wake of the scale model and full-scale mannequin despite an order-of-magnitude difference in Reynolds number. The drafting model shows that for spacings greater than a bike length, the trailing rider has negligible effect on the wake of the upstream rider.}, keywords = {}, pubstate = {published}, tppubtype = {inproceedings} } To improve the aerodynamic performance of cyclists, detailed information of the flow field is required around these highly three-dimensional bluff-body geometries. Using traditional measurement techniques with cyclists in a wind tunnel, it is often difficult or impractical to acquire detailed flow field surveys. In this paper two examples are discussed where highresolution Particle Image Velocimetry has been undertaken in a water channel to investigate the wake dynamics of a single pedalling cyclist and the flow between multiple cyclists. These areas have previously been difficult to measure experimentally using intrusive measurement techniques. The first example provides a comparison of the phase-averaged wake of a 1:4.5 scale pedalling cyclist/bicycle combination in the water channel and that of a full-scale cyclist mannequin of similar geometry and position in a wind tunnel. The second example shows an application of PIV to measure the flow field between two drafting cyclists. Good agreement is observed between the large-scale wake of the scale model and full-scale mannequin despite an order-of-magnitude difference in Reynolds number. The drafting model shows that for spacings greater than a bike length, the trailing rider has negligible effect on the wake of the upstream rider. |
![]() | Huang, Y; Venning, J; Thompson, M C; Sheridan, J Vortex separation and interaction in the wake of inclined trapezoidal plates Journal Article Journal of Fluid Mechanics, 771 , pp. 341–369, 2015. @article{Huang2015, title = {Vortex separation and interaction in the wake of inclined trapezoidal plates}, author = {Y Huang and J Venning and M C Thompson and J Sheridan}, url = {https://jamesvenning.net/wp-content/uploads/2015/11/JFM_Vortex_separation_and_interaction_in_the_wake_of_inclined_trapezoidal_plates.pdf}, doi = {10.1017/jfm.2015.160}, year = {2015}, date = {2015-01-01}, journal = {Journal of Fluid Mechanics}, volume = {771}, pages = {341--369}, publisher = {Cambridge University Press}, abstract = {Full three-dimensional numerical simulations are employed to investigate the flows over inclined trapezoidal low-aspect-ratio plates at low Reynolds numbers, aiming to understand the unsteadiness induced by the interaction between the trailing vortical wake structures originating from the swept edges, and those from the leading and trailing edges. The flows past eighteen different plate geometries in three broad sets are simulated to study the influence of aspect ratio, taper angle and angle of attack on the wake vortices and the force coefficients. Both taper ratio and angle of attack of plates with the same area are found to have a broadly predictable influence on the wake stability and asymptotic forces. Smaller taper ratios result in lower maximum lift, while an increase in the angle of attack results in a reduction in the differences in maximum lift. Two distinct modes of periodic unsteady flow with significant differences in frequency are observed. The corresponding vortex-shedding mechanisms are analysed with the aid of Q-criterion isosurfaces and streamlines. A low wake frequency is observed at small taper angles when there is relative independence between the von Kármán vortices originating from the leading and trailing edges, and weak swept-edge vortices. The dominant Strouhal number in this state is approximately 0.09. When the taper angle or angle of attack increases, the flows over the swept edges form stronger trailing vortex structures which interact strongly with the leading-edge vortices, combining to produce a regular stream of vortex loops shed into the wake. In this regime, the dominant Strouhal number increases to approximately 0.14-0.18. Higher Reynolds numbers and/or angles of attack result in a loss of centre plane reflection symmetry in the wake. The aerodynamic forces have been quantified as a function of the problem parameters and plate geometry. textcopyright 2015 Cambridge University Press.}, keywords = {}, pubstate = {published}, tppubtype = {article} } Full three-dimensional numerical simulations are employed to investigate the flows over inclined trapezoidal low-aspect-ratio plates at low Reynolds numbers, aiming to understand the unsteadiness induced by the interaction between the trailing vortical wake structures originating from the swept edges, and those from the leading and trailing edges. The flows past eighteen different plate geometries in three broad sets are simulated to study the influence of aspect ratio, taper angle and angle of attack on the wake vortices and the force coefficients. Both taper ratio and angle of attack of plates with the same area are found to have a broadly predictable influence on the wake stability and asymptotic forces. Smaller taper ratios result in lower maximum lift, while an increase in the angle of attack results in a reduction in the differences in maximum lift. Two distinct modes of periodic unsteady flow with significant differences in frequency are observed. The corresponding vortex-shedding mechanisms are analysed with the aid of Q-criterion isosurfaces and streamlines. A low wake frequency is observed at small taper angles when there is relative independence between the von Kármán vortices originating from the leading and trailing edges, and weak swept-edge vortices. The dominant Strouhal number in this state is approximately 0.09. When the taper angle or angle of attack increases, the flows over the swept edges form stronger trailing vortex structures which interact strongly with the leading-edge vortices, combining to produce a regular stream of vortex loops shed into the wake. In this regime, the dominant Strouhal number increases to approximately 0.14-0.18. Higher Reynolds numbers and/or angles of attack result in a loss of centre plane reflection symmetry in the wake. The aerodynamic forces have been quantified as a function of the problem parameters and plate geometry. textcopyright 2015 Cambridge University Press. |
![]() | Venning, J; Lo Jacono, D; Burton, D; Thompson, M C; Sheridan, J The effect of aspect ratio on the wake of the Ahmed body Journal Article Experiments in Fluids, 56 (126), 2015, ISSN: 1432-1114. @article{Venning2015, title = {The effect of aspect ratio on the wake of the Ahmed body}, author = {J Venning and D {Lo Jacono} and D Burton and M C Thompson and J Sheridan}, url = {https://jamesvenning.net/wp-content/uploads/2015/11/EXIF_The_effect_of_aspect_ratio_on_the_wake_of_the_Ahmed_body.pdf}, doi = {10.1007/s00348-015-1996-5}, issn = {1432-1114}, year = {2015}, date = {2015-01-01}, journal = {Experiments in Fluids}, volume = {56}, number = {126}, publisher = {Springer Berlin Heidelberg}, abstract = {This paper seeks to further elucidate the wake of the Ahmed body by investigating how the time-averaged flow structures vary with frontal aspect ratio. High-resolution particle image velocimetry results are provided for eight different width Ahmed geometries at Re√FA = 3 × 10^4 . It is shown that the narrower the body, the greater the downwash over the back slant, meaning the flow remains more attached. At a critical aspect ratio (AR = 1.9), the flow downstream changes. The separation over the back slant is shown to be affected by the AR, and this in turn has a significant effect on the circulation in the c-pillar vortices.}, keywords = {}, pubstate = {published}, tppubtype = {article} } This paper seeks to further elucidate the wake of the Ahmed body by investigating how the time-averaged flow structures vary with frontal aspect ratio. High-resolution particle image velocimetry results are provided for eight different width Ahmed geometries at Re√FA = 3 × 10^4 . It is shown that the narrower the body, the greater the downwash over the back slant, meaning the flow remains more attached. At a critical aspect ratio (AR = 1.9), the flow downstream changes. The separation over the back slant is shown to be affected by the AR, and this in turn has a significant effect on the circulation in the c-pillar vortices. |
2014 |
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![]() | Mcqueen, T; Venning, J; Sheridan, J Effects of Aspect Ratio on the Wake Dynamics of the Ahmed Body Inproceedings 19th Australasian Fluid Mechanics Conference, 2014, ISBN: 9780646596952. @inproceedings{Mcqueen2014, title = {Effects of Aspect Ratio on the Wake Dynamics of the Ahmed Body}, author = {T Mcqueen and J Venning and J Sheridan}, url = {https://jamesvenning.net/wp-content/uploads/2015/11/AFMC19_Effects_of_Aspect_Ratio_on_the_Wake_Dynamics_of_the_Ahmed_Body.pdf}, isbn = {9780646596952}, year = {2014}, date = {2014-01-01}, booktitle = {19th Australasian Fluid Mechanics Conference}, abstract = {Time-Resolved Particle Image Velocimetry (TR-PIV) data was acquired in the wake of Ahmed bodies allowing the effects of varying the aspect ratio on the wake dynamics to be revealed. The spatial structures and energy contained in the dominant wake modes within the frequency spectra were investigated. It was found that a dominant frequency existed in the near wake of all aspect ratio bodies and that this frequency appeared not to be influenced by aspect ratio. This frequency was related to an alternate vertical flapping motion of the C-pillar vortices. The influence of aspect ratio on the corner vortex strength was identified. The formation of a vortex below the C-pillar vortex that appeared dependent on the interaction between the upwash and downwash was also noted.}, keywords = {}, pubstate = {published}, tppubtype = {inproceedings} } Time-Resolved Particle Image Velocimetry (TR-PIV) data was acquired in the wake of Ahmed bodies allowing the effects of varying the aspect ratio on the wake dynamics to be revealed. The spatial structures and energy contained in the dominant wake modes within the frequency spectra were investigated. It was found that a dominant frequency existed in the near wake of all aspect ratio bodies and that this frequency appeared not to be influenced by aspect ratio. This frequency was related to an alternate vertical flapping motion of the C-pillar vortices. The influence of aspect ratio on the corner vortex strength was identified. The formation of a vortex below the C-pillar vortex that appeared dependent on the interaction between the upwash and downwash was also noted. |














