Chapter 2 lecture notes Flashcards

1
Q

Motion in the atmospheric boundary layer is generally

A

turbulent.

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2
Q

Most turbulent flows of interest, including those in the ABL have a number of common characteristics:

A
  • the flows are rotational and three dimensional (vorticity fluctuations are therefore important);
  • the flows are dissipative, so that energy must be supplied to maintain the turbulence;
  • (iii) the fluid motions are unpredictable in detail;
  • (iv) the rates of transfer and mixing are several orders of magnitude greater than the rate of molecular diffusion
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3
Q

Non-turbulent flows are called

A

laminar. In laminar flow, a perfect frictionless fluid would experience no tangential force at a boundary.

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4
Q

Non-turbulent flows are called laminar. In laminar flow, a perfect frictionless fluid would experience no tangential force at a boundary.

ļƒ˜ In contrast, a real fluid experiences

A

such tangential forces.

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5
Q

Such tangential forces are also referred to as

A

shearing stresses that are related to the fluid viscosity,

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6
Q

the frictional shearing stress unit

A

(frictional force per unit area) in Nm-2

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7
Q

the dynamic viscosity unit

A

kgm-1s-1

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8
Q

If we measure the flow with a fast-responding anemometer, we will find that the velocity

A

fluctuates with time in a seemingly random manner. Air temperature, humidity, and other scalars also exhibit irregular temporal fluctuations.

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9
Q

Details of the flow are

A

impossible to predict

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10
Q

Details of the flow are impossible to predict. Hence

A

we quantify the mean state of the atmosphere by performing averaging operation on the atmospheric properties

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11
Q

This averaging operation is called

A

block averaging

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12
Q

In field observations or modeling studies, time series data are obtained at

A

discrete sampling intervals, tf

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13
Q

In field observations or modeling studies, time series data are obtained at

discrete sampling intervals, tf . This interval is

A

constant in field measurements but can be variable in modeling studies.

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14
Q

A typical averaging length is

A

30 min

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15
Q

a typical sampling interval is

A

0.1 s

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16
Q

the molecular friction force are now expressed with

A

mean flow quantities

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17
Q

The extra terms in the parentheses consist of

A

spatial derivatives of Reynolds variances (e.g., -uā€™2) and covariances (e.g., -š‘¢ā€™š‘£ā€²). Like molecular friction, these terms act as retarding forces on the mean motion. Thus, a consequence of velocity fluctuations is that they slow down the air motion.

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18
Q

Resulting from averaging of the nonlinear terms, such as š‘¢ šœ•š‘¤ā„šœ•š‘§ , in the original equations, the Reynolds velocity covariances represent

A

turbulent momentum fluxes or transport of momentum by turbulent eddies.

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19
Q

Once again, the Reynolds averaging operation has produced additional terms.

ļƒ˜ These terms consist of

A

spatial derivatives of velocity-scalar covariances and are given in the parentheses on the right side of the equations.

20
Q

These terms consist of spatial derivatives of velocity-scalar covariances and are given in the parentheses on the right side of the equations.

ļƒ˜ In analogy to molecular diffusion, these covariances represent

A

turbulent transport of water vapor and potential temperature

21
Q

In other words, the result of velocity and scalar fluctuations is

A

a diffusive transport of energy and materials in the atmosphere.

22
Q

Turbulent transport is one factor contributing to

A

the local time rate of change in the mean scalar quantities.

23
Q

Other contributors of the temporal change are

A

horizontal and vertical advection and molecular diffusion (1st term on the right).

24
Q

Surface boundary conditions strongly affect

A

the vertical distributions of velocity, temperature, and gaseous abundance in the atmospheric boundary layer.

25
Q

The vertical gradients of these quantities are generally

A

much larger than their horizontal gradients

26
Q

From now on, we will also ignore the molecular terms because

A

they are much smaller in magnitude than their turbulent counterparts.

27
Q

To study flow dynamics in a neutral boundary layer,

A

the two momentum equations (Eqns. 10 and 11) will suffice. I

28
Q

In neutral stability,

A

turbulence is generated by vertical wind shear, and buoyancy does not play a role.

29
Q

If the atmosphere is stratified, or if we are interested in heat and water vapor transport,

A

we will also need Eqns. 13 and 14 to account for buoyancy generation and destruction of turbulence and to quantify the transport processes.

30
Q

A fundamental challenge in the studies of turbulent flow is

A

that the number of unknowns exceeds the number of mean equations

31
Q

This closure problem arises from

A

the fact Reynolds averaging generates variances and covariances from nonlinear terms in the instant equations.

32
Q

The additional equations, called turbulence closure parameterizations, are not derived from fundamental laws of thermodynamics and physics. Rather they are

A

empirical equations

33
Q

The most common parameterization scheme relates a

A

Reynolds covariance to the spatial gradient of the relevant mean quantity.

34
Q

The free parameter in these equations, K, is termed eddy diffusivity, having the dimensions of

A

m2 s-1

35
Q

The parameterizing equations 15ā€“18 state that the

A

strength of turbulent diffusion is proportional to the spatial gradient of the mean state quantity of interest

36
Q

The negative sign in these equations ensures that

A

the diffusion flux is directed down the gradient from a position of higher to a position of lower momentum, temperature, or gaseous concentration.

37
Q

The negative sign means a ā€¦ā€¦ā€¦ typically for ā€¦ā€¦ā€¦..

A

downward heat flux, from hot to cold. This is typical for statically stable ABL

38
Q

Kinetic energy is the

A

energy of motion

39
Q

These kinetic energy quantities are in dimensions of

A

m2s-2

40
Q

To obtain kinetic energy density in the familiar SI energy units of

A

Jm-3

41
Q

These kinetic energy quantities are in dimensions of m2s-2. To obtain kinetic energy density in the familiar SI energy units of Jm-3, we should

A

multiply them by the air density šœŒ in kgm-3.

42
Q

The TKE is

A

the smallest of all the energies (IE, APE, TKE and EKE) in the atmosphere.

43
Q

The total TKE in the atmospheric boundary layer is about

A

300 Jm-2

44
Q

The TKE in the air column above the boundary layer may be probably

A

several times smaller than the TKE in the boundary layer

45
Q

ā€¦ā€¦ā€¦ā€¦ā€¦ā€¦ā€¦ā€¦ā€¦ā€¦ā€¦ that makes the boundary layer uniquely different from the rest of the atmosphere

A

It is this small energy