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Objective Discus Turbulence
Introduce Reynolds Navier Stokes Equations (RANS)
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Conservation Equations
y z x
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Turbulence Forced convection on flat plate
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Turbulence
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Size of eddies hurricane nozzle 2 in Eddy ~ 1/100 in ~200 miles
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Transition from laminar to turbulent flow
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Turbulence in the vicinity of human body
PT-Teknik.dk
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Example The figure below shows a turbulent boundary layer due to forced convection above the flat plate. The airflow above the plate is steady-state. Consider the points A and B above the plate and line l parallel to the plate. Point A y Flow direction Point A Point B line l For the given time step presented on the figure above plot the velocity Vx and Vy along the line l. b) Is the stress component txy lager at point A or point B? Why? c) For point B plot the velocity Vy as function of time.
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3-D
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Indoor airflow jet jet The question is: What we are interested in:
exhaust supply jet The question is: What we are interested in: main flow or turbulence? turbulent
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Energy Cascade Concept in Turbulence
Kinetic energy is continually being transferred from the mean flow to the turbulent motion by large-scale eddies The process of vortex stretching leads to a successive reduction in eddy size and to a steepening of velocity gradients between adjacent eddies. Eventually the eddies become so small that viscous dissipation leads to the conversion of kinetic energy into heat.
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Method for solving of Navier Stokes (conservation) equations
Analytical Define boundary and initial conditions. Solve the partial deferential equations. Solution exist for very limited number of simple cases. Numerical - Split the considered domain into finite number of volumes (nodes). Solve the conservation equation for each volume (node). Infinitely small difference finite “small” difference
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Numerical method Simulation domain for indoor air and pollutants flow in buildings 3D space Solve p, u, v, w, T, C Split or “Discretize” into smaller volumes
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Capturing the flow properties
2” nozzle Eddy ~ 1/100 in Mesh (volume) should be smaller than eddies ! (approximately order of value)
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Mesh size for direct Numerical Simulations (DNS)
~1000 ~2000 cells For 2D wee need ~ 2 million cells Also, Turbulence is 3-D phenomenon !
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Mesh size For 3D simulation domain 2.5 m Mesh size 0.1m → 50,000 nodes
3D space (room)
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We need to model turbulence!
Reynolds Averaged Navier Stokes equations
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First Methods on Analyzing Turbulent Flow
- Reynolds (1895) decomposed the velocity field into a time average motion and a turbulent fluctuation vx’ Vx - Likewise f stands for any scalar: vx, vy, , vz, T, p, where: From this class We are going to make a difference between large and small letters Time averaged component
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Time Averaging Operations
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Averaging Navier Stokes equations
Substitute into Navier Stokes equations Instantaneous velocity fluctuation around average velocity Average velocity Continuity equation: time Average whole equation: Average Average of average = average Average of fluctuation = 0
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