CFD - Modelling Turbulent Flows Flashcards

1
Q

Reynolds Number (Re)

A

A dimensionless number used to indicate whether a fluid flow is either laminar or turbulent

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2
Q

Critical Reynolds Number

A

The onset of turbulence/transition occurs at a critical value of Re = 2300.

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3
Q

General Definition of Re

A

The ratio of inertia forces to friction forces.

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4
Q

Common features in transition processes

A
  • Amplification of initially small disturbances
  • Development of areas with concentrated rotational structures
  • Formation of intense small-scale motions
  • Growth and merging of these areas into full turbulent flows
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5
Q

What affects the transition processes

A
  • Pressure Gradient
  • Disturbance Levels
  • Wall Roughness
  • Heat Transfer
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6
Q

Characteristics of Turbulence

A
  • Irregularity (random and chaotic): treated statistically rather than deterministically
  • Three-dimensional rotation, unsteady
  • Diffusivity: enhanced mixing and increased rates of mass, momentum, and energy transports in a flow
  • Dissipation of energy (Kinetic Energy to Internal Energy)
  • Multi-scale vortex structures in the turbulent fields
  • Energy cascades from large-scale to smaller scale structures
  • Mixing: turbulence increases the mixing of momentum and heat
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7
Q

Energy Cascade

A

Large-scale structures cascade down to small-scale structures

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8
Q

Kolmogorov Length Scale

A

Structures that are small enough that molecular diffusion becomes important and viscous dissipation of energy finally takes place.

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9
Q

Spectral Energy E(K). Units: (m^3/s^2)

A

Kinetic energy per unit mass per unit wave number of fluctuations around the wave number K.

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10
Q

Kolmogorov Microscales

A

The smallest scales presented in a turbulent flow where viscosity dominates and the turbulent kinetic energy is dissipated into heat.

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11
Q

Reynolds Decomposition

A

Defines flow property phi(t) at this point as the sum of a steady mean component “phi bar” and a time-varying fluctuating component phi ‘ (t).

phi(t) = “phi bar” + phi ‘ (t)

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12
Q

Kinetic Energy per unit mass of the turbulence at a given location

A

k = 1/2 x ui’ x ui’ = 1/2 x (u’^2 + v’^2 + w’^2

ui’ - time-averaged fluctuation in velocity

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13
Q

Turbulence Intensity Ti

A

The average r.m.s velocity divided by a reference mean flow velocity

Ti = sqrt(2k/3)/Vref

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14
Q

Reynolds Averaged Navier-Stokes (RANS)

A

Average the Navier-Stokes Equations in time and use a model to predict the extra terms that appear. Models all turbulent scales.

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15
Q

Large Eddy Simulation (LES)

A

Solve the Navier-Stokes Equations only for large turbulent scales and use a model to account for the small turbulent scales

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16
Q

Direct Numerical Simulation (DNS)

A

Solve the Navier-Stokes Equations for all turbulent scales.

17
Q

Number of Extra Transport Equations

A

Algebraic Turbulence Model (Mixing Length Model) - 0

Spalart-Allmaras Model/1 Eq Differential Turbulence Model - 1

K-Epsilon Model/K-Omega Model/Algebraic Stress Model - 2

Reynolds Stress Model/Second Moment Closure - 7

18
Q

Near-Wall Flows

A

For turbulent flows, the boundary layer can be divided into inner and outer regions:

Inner Region:
Wall
- Viscous Sublayer
- Buffer Layer
- Log-Law Layer
——————————
Outer Region

19
Q

Viscous Sublayer

A

A thin layer in contact with the wall, dominated by viscous effects, almost laminar.

0 < y+ < 5~8

u+ = y+

20
Q

Buffer Layer

A

A transitional layer between the other two.

5~8 < y+ < 30~70

21
Q

Log-Law Layer

A

Dominated by viscous and turbulent effects.

u+ = 1/k ln(y+) + B

30~70 < y+ < 500

22
Q

Non-Slip Condition

A

On the wall, the velocity is zero.

23
Q

y+

A

Non-dimensional wall coordinate

24
Q

u+

A

Wall parallel velocity non-dimensionalised with friction velocity