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Turbulence and Flow Dynamics Quiz

Total questions: 81

Worksheet time: 41mins

Name
Class
Date
1.

Which of the following is NOT a characteristic of turbulent flow?

a)

Unsteady motion

b)

Regular and predictable patterns

c)

Three-dimensionality

d)

Enhanced mixing of transported quantities

2.

What is the name of the process where energy is transferred from larger eddies to smaller eddies in turbulent flow?

a)

Reynolds Averaging

b)

Energy Dissipation

c)

Energy Cascade

d)

Vortex Breakdown

3.

Reynolds number is used to determine:

a)

Flow compressibility

b)

Laminar or turbulent nature of flow

c)

Temperature gradient in a fluid

d)

Density variation

4.

What is the typical critical Reynolds number for internal flow to become turbulent?

a)

Re > 500

b)

Re > 2,300

c)

Re > 1,000

d)

Re > 50,000

5.

Which of the following defines Reynolds number?

a)

(μ / ρUL)

b)

(ρUL / μ)

c)

(U² / gL)

d)

(F / A)

6.

What is the main goal of turbulence modeling in CFD?

a)

Increase computational time

b)

Solve molecular diffusion directly

c)

Approximate the effects of turbulence without resolving all scales

d)

Eliminate the need for boundary conditions

7.

What does RANS stand for?

a)

Reynolds Analyzed Navier-Stokes

b)

Rapid Anisotropic Numerical Solver

c)

Reynolds-Averaged Navier-Stokes

d)

Rotational Averaged Navier Scale

8.

In RANS modeling, the velocity U is decomposed into:

a)

Time and space

b)

Instantaneous and fluctuating components

c)

Turbulent and non-turbulent components

d)

Viscous and inertial components

9.

What is the mathematical expression for turbulent kinetic energy k?

a)

½(u'² + v'² + w'²)

b)

u + v + w

c)

μ∇²u

d)

ρU²

10.

The closure problem in turbulence modeling arises because:

a)

The Navier-Stokes equations are complete

b)

Turbulence introduces additional knowns

c)

Reynolds stresses introduce new unknowns

d)

The continuity equation becomes invalid

11.

Which hypothesis is used in eddy viscosity models to relate Reynolds stresses to mean flow?

a)

Navier Hypothesis

b)

Kolmogorov Hypothesis

c)

Boussinesq Hypothesis

d)

Prandtl Mixing Length Hypothesis

12.

Reynolds stress models (RSM) are more suitable for:

a)

Simple 2D laminar flows

b)

Isotropic turbulence

c)

Complex 3D flows with strong curvature and swirl

d)

Inviscid flows

13.

In turbulent flow simulations, specifying what kind of conditions at inlets is essential?

a)

Laminar slip conditions

b)

Inviscid boundary conditions

c)

Turbulence boundary conditions

d)

Pressure boundary conditions only

14.

Which type of modeling approach is required near walls in turbulent flows?

a)

Inviscid model

b)

Free-slip condition

c)

Near-wall modeling

d)

Laminar wall assumption

15.

What does the turbulent kinetic energy (k) represent?

a)

Potential energy in eddies

b)

Average fluid velocity

c)

Energy in turbulent velocity fluctuations

d)

Viscous dissipation rate

16.

In two-equation models, which quantities are solved?

a)

Pressure and density

b)

Temperature and velocity

c)

Turbulent kinetic energy (k) and dissipation ( or )

d)

Eddy viscosity and flow rate

17.

The Standard k-ε model is recommended for:

a)

Highly accurate separation flows

b)

Crude estimates of turbulence

c)

Swirling dominated flows

d)

Supersonic shock interactions

18.

Which two models are recommended for standard cases?

a)

RNG k-ε and Spalart-Allmaras

b)

Realizable k-ε and SST k-ω

c)

Standard k-ε and LES

d)

DES and DNS

19.

For precise wall resolution, especially flow separation or heat transfer, which model is preferred?

a)

RNG k-ε

b)

Standard k-ε

c)

SST k-ω

d)

Spalart-Allmaras

20.

Which approach has the highest computational cost per iteration?

a)

RANS

b)

LES

c)

DNS

d)

Standard k-ε

21.

Which model assumes isotropic turbulence for calculations?

a)

Reynolds Stress Model (RSM)

b)

Large Eddy Simulation (LES)

c)

Standard k-ε

d)

Direct Numerical Simulation (DNS)

22.

In which region does the velocity profile transition from linear to logarithmic behavior?

a)

Free stream

b)

Wake region

c)

Near-wall region

d)

Separation zone

23.

What is the typical range of y+ for the first cell when using wall functions?

a)

0 < y+ < 10

b)

10 < y+ < 30

c)

30 < y+ < 300

d)

300 < y+ < 500

24.

When the viscous sublayer needs to be resolved, what should the first cell's y+ value be?

a)

100

b)

1

c)

10

d)

50

25.

Which turbulence model is recommended when resolving the viscous sublayer?

a)

RNG k-ε

b)

Standard k-ε

c)

SST k-ω

d)

Realizable k-ε

26.

Which situation would make wall functions unsuitable?

a)

Smooth, steady external flow

b)

Flows with boundary layer separation

c)

High Reynolds number free stream flow

d)

Subsonic flow over a flat plate

27.

When using Enhanced Wall Treatment (EWT) with a k-ε model, the method is:

a)

y+ dependent and requires y+ = 1

b)

y+ insensitive and adapts to grid placement

c)

only valid for laminar flows

d)

only used with Reynolds Stress Models

28.

What are typical default values for turbulence at an inlet?

a)

Intensity = 1%, Viscosity Ratio = 1

b)

Intensity = 5%, Viscosity Ratio = 10

c)

Intensity = 10%, Viscosity Ratio = 50

d)

Intensity = 20%, Viscosity Ratio = 100

29.

Why perform a hand calculation of first cell height during pre-processing?

a)

To avoid computing the Reynolds number

b)

To ensure the first cell lies within the desired y+ range

c)

To save computational time

d)

To avoid using turbulence models

30.

What is the typical range of turbulence intensity for normal turbulent flows?

a)

0.1% to 1%

b)

1% to 5%

c)

5% to 10%

d)

10% to 20%

31.

For external flows, what is the recommended turbulent viscosity ratio?

a)

0.1-1

b)

1-10

c)

10-100

d)

100-200

32.

Which turbulence model is preferred for cases where the viscous sublayer needs to be resolved?

a)

Standard k-ε

b)

RNG k-ε

c)

SST k-ω

d)

Realizable k-ε

33.

Which turbulence model severely underpredicts the size of the separation bubble in flow over a blunt flat plate?

a)

Realizable k-ε

b)

RNG k-ε

c)

Reynolds Stress Model

d)

Standard k-ε

34.

Which turbulence model is best suited for applications with swirling flows?

a)

SST k-ω

b)

Realizable k-ε

c)

Standard k-ε

d)

Reynolds Stress Model (RSM)

35.

In the diffuser example, which model predicts flow separation more accurately?

a)

RNG k-ε

b)

SST k-ω

c)

Realizable k-ε

d)

Reynolds Stress Model

36.

What is the first step in solving the example problem using the Finite Volume Method (FVM)?

a)

Define boundary conditions

b)

Convert to algebraic form

c)

Start from the governing equation

d)

Choose the type of discretization

37.

In the Finite Volume Method, what does the general energy balance for each control volume include?

a)

Convection and conduction only

b)

Heat in from left and right, and a source term

c)

Only the source term

d)

Time-dependent terms

38.

What form must the energy balance equation be converted into to solve it numerically?

a)

Trigonometric form

b)

Exponential form

c)

Algebraic form

d)

Integral form

39.

In the context of the example, what is defined at each node?

a)

Temperature gradients

b)

Coefficients

c)

Boundary fluxes

d)

Volume integrals

40.

Which nodes have special treatment in this example?

a)

Node 2 and Node 4

b)

Node 1 and Node 5

c)

Node 3 and Node 4

d)

Node 1 and Node 3

41.

What type of boundary condition is applied at Node 1 in the example problem?

a)

Neumann boundary condition

b)

Dirichlet boundary condition

c)

Robin boundary condition

d)

Periodic boundary condition

42.

At Node 5, which of the following best describes the boundary condition?

a)

Fixed temperature

b)

Adiabatic (zero heat flux)

c)

Convective heat loss

d)

Uniform source term

43.

What is the role of the source term (S) in the general energy balance?

a)

To model conduction effects

b)

To represent heat addition or generation inside the control volume

c)

To enforce boundary conditions

d)

To ensure mass conservation

44.

In the finite volume formulation, what does the term typically represent?

a)

Flux across control surfaces

b)

Net energy storage

c)

Coefficient of the central node in the discretized equation

d)

Volume of the control element

45.

What is the purpose of defining coefficients , , and at each node?

a)

To simplify the geometry

b)

To improve accuracy of boundary conditions

c)

To structure the system of algebraic equations

d)

To enforce temperature constraints

46.

Why do we apply special treatment to boundary nodes in FVM?

a)

To avoid numerical instability

b)

Because they require integration over half control volumes

c)

They have no heat transfer

d)

To apply periodic constraints

47.

In the finite volume method (FVM), what is the key step that distinguishes it from other CFD techniques?

a)

Using staggered grids

b)

Integration over control volumes

c)

Assuming constant properties

d)

Applying boundary conditions manually

48.

What is the primary governing equation considered for one-dimensional steady-state diffusion in FVM?

a)

Navier-Stokes equation

b)

Bernoulli’s equation

c)

Diffusion equation

d)

Energy conservation equation

49.

In the notation used for grid points, what do P, W, and E represent?

a)

Pressure, Weight, Energy

b)

Present, Western, Eastern nodes

c)

Past, Western, Eastern control volumes

d)

Peak, Width, Elevation

50.

In central differencing, which approximation is used for gradients and interface values?

a)

Linear interpolation

b)

Quadratic approximation

c)

Taylor series expansion

d)

Finite difference method

51.

What does the coefficient aP represent in the discretized equations?

a)

Average pressure at node P

b)

Total flux at node P

c)

Sum of contributions from neighboring nodes and source terms

d)

Temperature difference at P

52.

What technique is commonly used to solve the resulting linear system of equations in FVM?

a)

Newton-Raphson method

b)

Gauss Elimination

c)

Runge-Kutta method

d)

Euler integration

53.

In a 2D diffusion problem, which of the following is not a neighboring node of P?

a)

North (N)

b)

Top (T)

c)

East (E)

d)

West (W)

54.

For a 3D control volume, how many neighboring nodes are associated with an internal node?

a)

4

b)

5

c)

6

d)

8

55.

How are boundary conditions typically incorporated in FVM?

a)

Ignored if source terms exist

b)

By introducing artificial nodes

c)

By modifying source terms and cutting links

d)

By increasing the mesh size

56.

What does the linearized source term allow in the discretized equations?

a)

Variable grid size

b)

Implicit treatment of source effects

c)

Neglect of boundary fluxes

d)

Direct calculation of node positions

57.

In the finite volume method, where are the control volume boundaries placed in a 1D grid?

a)

At the nodal points

b)

At the domain edges only

c)

Midway between adjacent nodes

d)

Randomly within the domain

58.

What is the physical interpretation of the discretized diffusion equation?

a)

Conservation of momentum

b)

Flux difference equals generation within control volume

c)

Constant temperature across the domain

d)

Heat loss equals temperature rise

59.

What is typically the first step in solving a diffusion problem using FVM?

a)

Apply boundary conditions

b)

Generate the grid

c)

Solve the algebraic system

d)

Define material properties

60.

In 2D FVM, what is the face area associated with the north and south faces of a control volume?

a)

Δy

b)

Δx

c)

Δx * Δy

d)

A constant value

61.

What is the key feature of the example involving a circular fin?

a)

Uniform internal heating

b)

Convective heat loss as a sink term

c)

No boundary condition at the base

d)

Nonlinear conductivity

62.

What is the governing equation in the circular fin example?

a)

d²T/dx² = 0

b)

d²T/dx² − hP(T − T∞)/kA = 0

c)

∇²T = 0

d)

∂T/∂t = α∇²T

63.

In the 1D conduction example (Example 4.1), the relation implies:

a)

Constant property values

b)

Conservation of energy

c)

Symmetric boundary conditions

d)

Fixed temperature

64.

What numerical method is suggested for solving the linear algebraic system?

a)

Jacobi method

b)

Gauss-Seidel method

c)

Gauss Elimination

d)

Multigrid method

65.

In Example 4.2, which physical phenomenon is modeled?

a)

Convective cooling

b)

Uniform heat generation in a plate

c)

Heat sink with variable conductivity

d)

Advection-diffusion

66.

In 3D FVM problems, how many control volume faces does an internal node have?

a)

3

b)

4

c)

6

d)

8

67.

The discretized equation for a node P in 3D involves which neighboring directions?

a)

Only East, West, North

b)

East, West, South, North

c)

All six directions: W, E, S, N, B, T

d)

Diagonal neighbors only

68.

What happens to the source terms at boundary nodes in FVM?

a)

They are eliminated

b)

They become zero

c)

They are modified to include boundary effects

d)

They are ignored

69.

The finite volume discretized equation has the general form:

a)

aPφP = aWφW + aEφE + Su

b)

∇φ = 0

c)

φP = φW + φE

d)

aP = Su + SpφP

70.

What grid refinement technique improves the accuracy of the numerical solution?

a)

Using higher-order time schemes

b)

Employing finer control volumes

c)

Ignoring boundary conditions

d)

Increasing the temperature difference

71.

Which software is suggested for plotting the final numerical results?

a)

MATLAB

b)

ANSYS Fluent

c)

Tecplot

d)

Excel

72.

What is the first step in solving the example diffusion problem using the finite volume method?

a)

Apply boundary conditions

b)

Solve the matrix equation

c)

Start from the governing equation

d)

Define nodal temperatures

73.

In the energy balance for a control volume, what terms are considered?

a)

Kinetic energy and potential energy

b)

Heat conduction only

c)

Heat in from west, heat in from east, and source term

d)

Convection, radiation, and mass flow

74.

What is the result of discretizing the governing equation using the finite volume method?

a)

A differential equation

b)

A matrix of second derivatives

c)

An algebraic equation

d)

A Fourier series

75.

What is the key feature of the discretized form at each node?

a)

It includes velocity terms

b)

It excludes the source term

c)

It is based on energy conservation

d)

It varies for each time step

76.

Which nodes require special treatment in the discretized system?

a)

Interior nodes only

b)

Nodes at the top and bottom

c)

Node 1 and Node 5 (boundary nodes)

d)

Even-numbered nodes only

77.

In the example problem, what type of boundary condition is typically applied at Node 1?

a)

Adiabatic

b)

Fixed temperature (Dirichlet)

c)

Convective

d)

Insulated

78.

What modification is made to the coefficients at boundary nodes?

a)

They are averaged

b)

They are doubled

c)

They are adjusted to include boundary contributions

d)

They are zeroed

79.

What method is used to calculate temperature at each node after forming the equations?

a)

Numerical integration

b)

Finite element iteration

c)

Solving a system of linear equations

d)

Curve fitting

80.

In the general energy balance for FVM, if there is no source term, what is the balance?

a)

Heat in = Heat out

b)

Heat in from west = Heat in from east

c)

Heat in from both sides = 0

d)

Sum of heat in = 0

81.

Which part of the FVM process converts physical principles into solvable algebraic equations?

a)

Boundary condition application

b)

Integration over the domain

c)

Discretization step

d)

Initial condition setting