Dr Zaman Kamruzzaman
Adjunct Associate Lecturer
School of Engineering
- Email:md.kamruzzaman@newcastle.edu.au
- Phone:(02) 49854938
Career Summary
Biography
Dr. Kamruzzaman is working currently as an Associate Lecturer at the School of Engineering, Faculty of Engineering, and Built Environment. He obtained his
He is an expert in Turbulent flows (Turbulent boundary layer, Channel flow, plane jet, mixing turbulent layers, and grid turbulence). He is also familiar with ANSYS-Fluent and OpenFoam.
He is also interested in teaching fluid mechanics and heat and mass transfer, Magnetohydrodynamics, Thermodynamics, and Aerodynamics. Furthermore, Dr. Zaman also worked as an Assistant Professor at the American International University Bangladesh for almost one year teaching Calculus, Fluid Mechanics, and Mathematical Modelling. He also worked as a casual teacher at Deakin University and RMIT University in Australia.
Dr. Zaman published his research work in high-ranked international journals relevant to fluid mechanics. He also achieved a Pilot Strategic Grant from the University of Newcastle in 2017. He also worked on several projects as a consultant for wind services in high-rise buildings in Australia.
Teaching Interest: Fluid Mechanics, Turbulent flows, Aerodynamics, Thermodynamics, Heat and Mass Transfer, Calculus, Differential Equations, Mathematical Modelling, Computational Fluid Dynamics.
Software Knowledge: Matlab, Ansys, OpenFoam, Solid Works, MS Office,
Experimental tools: PIV, Hot-wire Anemometry.
Qualifications
- Doctor of Philosophy, University of Newcastle
- Bachelor of Science, Khulna University - Bangladesh
- Master of Mathematics, Khulna University - Bangladesh
Keywords
- Ansys and OpenFoam
- Building Aerodynamics
- Computational Fluid Mechanics
- Fluid Mechanics
- Heat and Mass Transfer
- Jet turbulence
- Magnetohydrodynamics
- Numerical Analysis
- Plane jet
- Turbulent Boundary Layer
- Turbulent Channel Flow
- Turbulent Flow Control
- Turbulent Shear and Shearless Mixing Layer
Languages
- Bengali (Mother)
- English (Fluent)
Fields of Research
Code | Description | Percentage |
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401206 | Fluid-structure interaction and aeroacoustics | 30 |
401213 | Turbulent flows | 50 |
401204 | Computational methods in fluid flow, heat and mass transfer (incl. computational fluid dynamics) | 20 |
Professional Experience
Academic appointment
Dates | Title | Organisation / Department |
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14/2/2019 - 30/8/2021 |
Postdoctoral Research Fellow I have worked at NUTNU to investigate the effects of upcoming turbulence on the mixing of helium gas and air flow in a 2D turbulent channel flow using PIV.
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Norwegian University of Science and Technology (NTNU) Department of Energy and Process Engineering Norway |
24/9/2017 - 28/2/2019 |
Assistant ProfessorOverview of American International University-Bangladesh (AIUB)American International University - Bangladesh (AIUB) is a Vision
Mission
Quality Policy
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American International University Bangladesh Mathematics Bangladesh |
Professional appointment
Dates | Title | Organisation / Department |
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16/6/2021 - 16/11/2021 |
Senior Wind Engineer Building Aerodynamics.
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Global Wind Technology Services Pty Ltd Consultancy Australia |
2/5/2016 - 17/5/2018 |
Resarch Assistant Research Assistant: Pursued fundamental research to study the small-scale turbulence in grid generated turbulence using classical and composite grids (shear and shearless mixing layers) and 2D rough wall boundary layer under the supervision of Prof. Lyazid Djenidi and Emeritus Prof. R.A.Antonia. For the first time, shearless and shear mixing layer turbulent flows are being investigated by using a tailor made the composite grid as a part of my current research. Key responsibilities: • Wind tunnel design and modification. • Wind tunnel testing. • Hot-wire probe build. • Measurements. • Data collection and analysis. • Computer coding. • Formulating new ideas and solving Mathematical problems. • Numerical analysis. • Preparing oral presentation for the international conferences. • Publishing journal papers. |
Faculty of Engineering and Built Environment - The University of Newcastle (Australia) Mechanical Engineering Australia |
Teaching
Code | Course | Role | Duration |
---|---|---|---|
SIT 192 |
Discrete Mathematics, Deakin University Deakin University Tutor |
Tutor | 1/1/0001 - 31/12/2022 |
MATH2310 |
Faculty of Mathematics and Physical Science The University of Newcastle - Faculty of Science and Mathematics Tutoring |
Casual Academic and Tutor | 15/5/2018 - 31/12/2018 |
SIT 190 |
Introduction to Functions, Relations and Graphs Deakin University Lecturing |
Visitor | 1/1/0001 - 31/12/2022 |
SIT 191 |
Applied Algebra and Statistics, Deakin University Deakin University Tutoring |
Tutor | 24/2/2022 - 4/7/2022 |
MATH 1142 |
Calculus and Analysis, Mathematics Department, RMIT RMIT University Tutoring and Marking |
Sessional Lecturer | 24/2/2020 - 31/7/2020 |
MECH-2700 |
Thermo and Fluid Dynamics Faculty of Engineering and Built Environment - The University of Newcastle (Australia) Tutoring to the undergraduate students |
Casual academic faculty | 24/7/2017 - 24/12/2017 |
Publications
For publications that are currently unpublished or in-press, details are shown in italics.
Journal article (17 outputs)
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2023 |
Kamruzzaman MD, Djenidi L, Antonia RA, 'Experimental study of two side-by-side decaying grid turbulent fields at different mean velocities', JOURNAL OF TURBULENCE, 24 (2023) [C1]
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2022 |
Asadi M, Kamruzzaman M, Hearst RJ, 'Structure of turbulent channel flow subjected to simultaneous inlet turbulence and localized injection', PHYSICAL REVIEW FLUIDS, 7 (2022) [C1]
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2022 |
Asadi M, Kamruzzaman M, Hearst RJ, 'The effect of inlet turbulence on the quiescent core of turbulent channel flow', Journal of Fluid Mechanics, 935 (2022) [C1] The impact of inlet turbulence on the structure of turbulent channel flow is investigated using particle image velocimetry. Streamwise-wall-normal plane measurements are performed... [more] The impact of inlet turbulence on the structure of turbulent channel flow is investigated using particle image velocimetry. Streamwise-wall-normal plane measurements are performed in a channel, where different turbulence intensities were generated at the inlet with an active grid. Four cases are tested with matched centreline mean velocities, while the centreline turbulence intensities ranged from 3.7 % for the reference case, up to 6.4 %. The friction velocity is found to be approximately constant with varying centreline turbulence intensities, resulting in a matched friction Reynolds number of for all cases, which contrasts with similar experiments performed in a zero-pressure-gradient boundary layer. The log region remains intact for all cases. The so-called quiescent core of the turbulent channel flow is also investigated. In addition to increased core discontinuity, the increased fluctuations of the streamwise velocity give rise to new core states, which differ from the conventional ones in their characteristic velocity. They are associated with a bulk of low- or high-momentum fluid passing through the measurement domain, and their occurrence increases with turbulence intensity. Tracking the core boundaries indicates an overall tendency of the core to move closer to the wall for increased inlet turbulence intensities, resulting in an increased core thickness. Moreover, it is found that the low-momentum cores generally reside closer to the wall compared with the ordinary cores and appear to be thicker than them, whereas the opposite, i.e. residing farther from the wall and being thinner, is true for the high-momentum cores.
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2021 |
Kamruzzaman M, Romcke O, Hearst RJ, 'The impact of upstream turbulence on a plane jet', EXPERIMENTS IN FLUIDS, 62 (2021) [C1]
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2021 |
Kamruzzaman M, 'Modified transport equation for the turbulent kinetic energy dissipation of the grid turbulence in the transition period of decay', JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 43 (2021) [C1]
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2021 |
Kamruzzaman M, Djenidi L, Antonia RA, 'Study of the interaction of two decaying grid-generated turbulent flows', Physics of Fluids, 33 (2021) [C1]
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2019 |
Djenidi L, Kamruzzaman M, Dostal L, 'Effects of wall suction on a 2D rough wall turbulent boundary layer', Experiments in Fluids, 60 (2019) [C1]
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2018 |
Kamruzzaman M, Djenidi L, Antonia RA, 'Behaviour of the energy dissipation coefficient in a rough wall turbulent boundary layer', Experiments in Fluids, 59 (2018) [C1]
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2017 |
Djenidi L, Lefeuvre N, Kamruzzaman M, Antonia RA, 'On the normalized dissipation parameter C-epsilon in decaying turbulence', JOURNAL OF FLUID MECHANICS, 817 61-79 (2017) [C1]
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2016 |
Talluru KM, Djenidi L, Kamruzzaman M, Antonia RA, 'Self-preservation in a zero pressure gradient rough-wall turbulent boundary layer', JOURNAL OF FLUID MECHANICS, 788 57-69 (2016) [C1]
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2015 |
Kamruzzaman M, Djenidi L, Antonia RA, Talluru KM, 'Scale-by-scale energy budget in a turbulent boundary layer over a rough wall', International Journal of Heat and Fluid Flow, (2015) [C1] Hot-wire velocity measurements are carried out in a turbulent boundary layer over a rough wall consisting of transverse circular rods, with a ratio of 8 between the spacing (w) of... [more] Hot-wire velocity measurements are carried out in a turbulent boundary layer over a rough wall consisting of transverse circular rods, with a ratio of 8 between the spacing (w) of two consecutive rods and the rod height (k). The pressure distribution around the roughness element is used to accurately measure the mean friction velocity (Ut) and the error in the origin. It is found that Ut remained practically constant in the streamwise direction suggesting that the boundary layer over this surface is evolving in a self-similar manner. This is further corroborated by the similarity observed at all scales of motion, in the region 0.2=y/d=0.6, as reflected in the constancy of Reynolds number (R¿) based on Taylor's microscale and the collapse of Kolmogorov normalized velocity spectra at all wavenumbers.A scale-by-scale budget for the second-order structure function <(du)2> (du=u(x+r)-u(x), where u is the fluctuating streamwise velocity component and r is the longitudinal separation) is carried out to investigate the energy distribution amongst different scales in the boundary layer. It is found that while the small scales are controlled by the viscosity, intermediate scales over which the transfer of energy (or <(du)3>) is important are affected by mechanisms induced by the large-scale inhomogeneities in the flow, such as production, advection and turbulent diffusion. For example, there are non-negligible contributions from the large-scale inhomogeneity to the budget at scales of the order of ¿, the Taylor microscale, in the region of the boundary layer extending from y/d=0.2 to 0.6 (d is the boundary layer thickness).
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2015 |
Djenidi L, Kamruzzaman M, Antonia RA, 'Power-law exponent in the transition period of decay in grid turbulence', JOURNAL OF FLUID MECHANICS, 779 (2015) [C1]
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2015 |
Kamruzzaman M, Djenidi L, Antonia RA, Talluru KM, 'Drag of a turbulent boundary layer with transverse 2D circular rods on the wall', EXPERIMENTS IN FLUIDS, 56 (2015) [C1]
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2014 |
Wahiduzzaman M, Kamruzzaman M, Alam MM, Ferdows M, 'Magnetic field effect on fluid flow through a rotating rectangular straight duct with large aspect ratio', PROGRESS IN COMPUTATIONAL FLUID DYNAMICS, 14 398-405 (2014) [C1]
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2013 |
Kamruzzaman M, Wahiduzzaman M, Alam MM, Djenidi L, 'The effects of magnetic field on the fluid flow through a rotating straight duct with large aspect ratio', Procedia Engineering, 56 239-244 (2013) [C1] This paper presents a numerical study of an investigation of a fluid flow through a rotating rectangular straight duct in the presence of magnetic field. The straight duct of rect... [more] This paper presents a numerical study of an investigation of a fluid flow through a rotating rectangular straight duct in the presence of magnetic field. The straight duct of rectangular cross-section rotates at a constant angular velocity about the centre of the duct cross-section is same as the axis of the magnetic field along the positive direction in the stream wise direction of the flows. Numerical calculation is based on the Magneto hydrodynamics incompressible viscous steady fluid model whereas Spectral method is applied as a main tool. Flow depends on the Magnetic parameter, Dean number and Taylor number. One of the interesting phenomena of the fluid flow is the solution curve and the flow structures in case of rotation of the duct axis. The calculation are carried out for 5 = Mg = 50000, 50 = Tr 100000, Dn 500, 1000, 1500 and 2000 where the aspect ratio ¿ 3.0. The maximum axial flow will be shifted to the centre from the wall and turn into the ring shape under the effects of high magnetic parameter and large Taylor number whereas the fluid particles strength is weak. © 2013 The Authors. Published by Elsevier Ltd.
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2013 |
Wahiduzzaman M, Kamruzzaman M, Alam MM, Ferdows M, 'Magnetic effect on direct numerical simulations of fluid flow through a rotating rectangular straight duct', INTERNATIONAL JOURNAL OF APPLIED ELECTROMAGNETICS AND MECHANICS, 42 327-342 (2013) [C1]
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Show 14 more journal articles |
Conference (12 outputs)
Year | Citation | Altmetrics | Link | ||||||||
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2022 |
Asadi M, Kamruzzaman M, Jason Hearst R, 'THE QUIESCENT CORE OF TURBULENT CHANNEL FLOW UNDER THE INFLUENCE OF INLET TURBULENCE', 12th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2022 (2022) The quiescent core of turbulent channel flow is examined under the influence of inlet turbulence using planar particle image velocimetry. Four cases are tested with matched center... [more] The quiescent core of turbulent channel flow is examined under the influence of inlet turbulence using planar particle image velocimetry. Four cases are tested with matched centerline mean velocities, while the centerline turbulence ranged from 3.7% for the reference case, up to 6.4% for the most turbulent case. A matched friction Reynolds number of Ret ¿ 770 is found for all cases, which contrasts with similar measurements in a zero-pressure-gradient boundary layer where Ret varies with freestream turbulence. The added turbulence increases the frequency of core discontinuity inside the channel and gives rise to new core types. The new cores differ from the conventional ones in their characteristic velocity, while their occurrence increases with turbulence intensity. They are associated with a bulk of low- or high-momentum fluid passing through the measurement domain. Their presence in the channel implies a more turbulent state of the flow inside the core region. It is also observed that, under the effect of increased inlet turbulence intensities, the core boundary moves closer to the wall, which yields thicker cores.
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2022 |
Kumbhar S, Djenidi L, Ghanadi F, Kamruzzaman M, 'THE EFFECT OF LARGE EDDY BREAK-UP DEVICE ON ROUGH WALL TURBULENT BOUNDARY LAYER', 12th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2022 (2022) The effect of large eddy break up (LEBU) device on the rough wall turbulent boundary layer up to Re¿ ¿ 12000 is investigated using hot-wire anemometry. The pressure measurements (... [more] The effect of large eddy break up (LEBU) device on the rough wall turbulent boundary layer up to Re¿ ¿ 12000 is investigated using hot-wire anemometry. The pressure measurements (around a circular roughness element) are carried out to determine skin-friction coefficient (cf) and friction velocity (Ut). The LEBU is flat plate, installed at wall normal distance of 0.8d (local boundary layer thickness) from the wall. The LEBU effect is observed immediate downstream of the device, where it creates a region of recirculating wake. At 43.7LB (LB is the LEBU chord length), maximum LEBU effect is reflected in the reduction in turbulence intensity. The boundary layer recovers around 50.4LB
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2019 |
Kamruzzaman M, Djenidi L, Antonia RA, 'Scale-by-scale assessment of the effects of mean shear on the energy budget in decaying turbulence', 11th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2019, Southampton, UK (2019) [E1]
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2016 |
Kamruzzaman M, Djenidi L, Antonia RA, 'Turbulent Sheared Mixing Layer Generated with a Composite Grid', FLUID-STRUCTURE-SOUND INTERACTIONS AND CONTROL, Perth, AUSTRALIA (2016) [E1]
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2016 |
Djenidi L, Kamruzzaman M, Antonia RA, 'Energy Dissipation rate parameter in a rough wall turbulent boundary layer', 20th Australasian Fluid Mechanics Conference, Perth, W.A. (2016) [E1]
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2015 |
Kamruzzaman M, Djenidi L, Antonia RA, 'Shearless mixing layer in grid generated turbulence at moderate Reynolds number', 9th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2015 (2015) The decay of turbulence in a shearless mixing layer generated from the junction of side by side grids with different mesh sizes but identical solidity is being investigated using ... [more] The decay of turbulence in a shearless mixing layer generated from the junction of side by side grids with different mesh sizes but identical solidity is being investigated using hot wire anemometry. It is observed that turbulence decays according to a power-law, albeit, with a different power-law exponent (n) for each grid. The measurements suggest the existence of turbulent energy transfer from the larger mesh region to the smaller mesh region at distances as large as 75 ML from the grid, where ML is the mesh size of the larger mesh grid. It is further observed that the Reynolds number R¿ remains constant along the centreline of the flow (i.e. the junction of the two grids), confirming that self-preservation is satisfied in this region of the flow. This is supported by the one dimensional velocity spectra Eu(k1). On the centreline, the measured energy spectra at positions x/ML = 45 collapse onto a single curve at all wavenumbers when scaled by either the Kolmogorov velocity and length scales or the rms velocity (u!) and Taylor microscale (X). Away from the centreline the spectra do not present such collapse.
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2015 |
Talluru KM, Kamruzzaman M, Djenidi L, Antonia RA, 'Self-preservation in zero pressure gradient turbulent boundary layers', 9th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2015 (2015) Starting with the Navier-Stokes Equation (NSE), we derived the conditions for self-preservation (SP) in a zeropressure gradient (ZPG) turbulent boundary layer. The analysis showed... [more] Starting with the Navier-Stokes Equation (NSE), we derived the conditions for self-preservation (SP) in a zeropressure gradient (ZPG) turbulent boundary layer. The analysis showed that it is strictly not possible to obtain SP in a ZPG turbulent boundary layer, unless the viscous term is eliminated from the NSE. This can be achieved in a smooth wall boundary layer only when the Reynolds number (Re) approaches infinity. In the case of rough walls, it is noted that the viscous effects can be compensated by surface roughness and therefore, SP is achievable, irrespective of Re. In this case, SP analysis showed that velocity scale (u*) must be constant and the length scale (l) should vary linearly with streamwise distance (x). These SP conditions are tested using experimental data taken over a similar streamwise fetch on a smooth wall and several types of rough walls. It is observed that complete SP in a ZPG turbulent boundary layer is possible when the roughness height (¿) increases linearly with x, where both the SP constraints (u* =UT = constant and l = d ¿ x) are met. In the present rough wall study, UT is observed to remain practically constant in x and d ~ x and appears to be the next best candidate for achieving SP.
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2014 |
Kamruzzaman M, Djenidi L, Antonia RA, 'Effects of low Reynolds number on decay exponent in grid turbulence', Procedia Engineering (2014) [E1] This present work is to investigate on the decay exponent (n) of decay power law (q' 2~(t - To)n , q'2 is the total turbulent kinetic energy, t is the decay time, t0 is ... [more] This present work is to investigate on the decay exponent (n) of decay power law (q' 2~(t - To)n , q'2 is the total turbulent kinetic energy, t is the decay time, t0 is the virtual origin) at low Reynolds numbers based on Taylor microscale R¿(= u '¿/ v) = 64 . Hot wire measurements are carried out in a grid turbulence subjected to a 1.36:1 contraction. The grid consists in large square holes (mesh size 43.75 mm and solidity 43%); small square holes (mesh size 14.15mm and solidity 43%) and woven mesh grid (mesh size 5mm and solidity 36%). The decay exponent (n) is determined using three different methods: (i) decay of q'2, (ii) transport equation for s , the mean dissipation of the turbulent kinetic energy and (iii) ¿ method (Taylor microscale ¿ = v5( q2)/ (ed)} , angular bracket denotes the ensemble). Preliminary results indicate that the magnitude n increases while R¿ (= u'¿/v)decreases, in accordance with the turbulence theory.
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2014 |
Kamruzzaman M, Talluru KM, Djenidi L, Antonia RA, 'An experimental study of turbulent boundary layer over 2D transverse circular bars', Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014 (2014) In this paper, we present the results from a turbulent boundary layer developing over a rough surface. The surface consists of transverse cylindrical rods (k, the rod diameter) th... [more] In this paper, we present the results from a turbulent boundary layer developing over a rough surface. The surface consists of transverse cylindrical rods (k, the rod diameter) that are periodically arranged in the streamwise direction with a spacing of ¿/k = 8 (¿ is the distance between two adjacent roughness elements), that results in maximum form drag. Particular attention is paid to the measurement of the friction velocity (Ut) that plays a major role in the assessment of the roughness effects on the flow. Hot-wire anemometry is used to measure the mean and fluctuating velocity components and pressure tap measurements are carried out to obtain the drag. Two methods are used to determine Ut. One is based on the momentum integral equation. The second relies on measuring the pressure distribution around one roughness element. Results show that both methods give consistent values for Ut to within 3%. Further, the drag coefficient (CD) is observed to be independent of the Reynolds number.
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Grants and Funding
Summary
Number of grants | 1 |
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Total funding | $20,000 |
Click on a grant title below to expand the full details for that specific grant.
20171 grants / $20,000
Effects of wall suction rate over a 2D transverse rod in the rough wall turbulent boundary layer.$20,000
Funding body: Faculty of Engineering and Built Environment - The University of Newcastle (Australia)
Funding body | Faculty of Engineering and Built Environment - The University of Newcastle (Australia) |
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Project Team | Md Kamruzzaman; Prof. Lyazid Djenidi |
Scheme | FEBE Strategic Pilot Grant |
Role | Lead |
Funding Start | 2017 |
Funding Finish | 2017 |
GNo | |
Type Of Funding | Internal |
Category | INTE |
UON | N |
Research Supervision
Number of supervisions
Current Supervision
Commenced | Level of Study | Research Title | Program | Supervisor Type |
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2021 | PhD |
Rough wall turbulent boundary layer subjected to LEBU. Rough Wall turbulent boundary is investigated and subjected to the LEBU in terms of drag reduction. |
Mechanical Engineering, Faculty of Engineering and Built Environment- The University of Newcastle | Co-Supervisor |
Past Supervision
Year | Level of Study | Research Title | Program | Supervisor Type |
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2023 | Honours |
The effects of incoming turbulence on the roughened cylinder to investigate the drag coefficient. Rough cylinder and grid turbulence |
Mechanical Engineering, Faculty of Engineering and Built Environment- The University of Newcastle | Principal Supervisor |
2022 | Honours |
Incoming turbulence effects on the smooth cylinder. Smooth Cylinder and grid turbulence |
Mechanical Engineering, Faculty of Engineering and Built Environment- The University of Newcastle | Principal Supervisor |
2020 | Honours |
Effects of roughness on the cylinder using ANSYS-FLUENT Co supervisor |
Aerospace Eng & Technology, UTS | Co-Supervisor |
2018 | Honours |
Rough wall turbulent boundary layer response to wall suction Co-supervisor |
Mechanical Engineering, Department of Mechanical Engineering | Co-Supervisor |
2017 | Honours | The effects of wall suction on the turbulent boundary layer | Mechanical Engineering, Faculty of Engineering and Built Environment - The University of Newcastle (Australia) | Co-Supervisor |
2015 | Masters |
Grid generated turbulent shearless mixing layer Co-Supervisor |
Mechanical Engineering, Department of Mechanical Engineering | Co-Supervisor |
Dr Zaman Kamruzzaman
Position
Adjunct Associate Lecturer
Turbulence Research Group
School of Engineering
College of Engineering, Science and Environment
Contact Details
md.kamruzzaman@newcastle.edu.au | |
Phone | (02) 49854938 |
Mobile | +610480240404 |
Links |
Research Networks Research Networks Research Networks Research Networks |
Office
Room | TA-204 |
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Building | TA Building |
Location | Callaghan University Drive Callaghan, NSW 2308 Australia |