Title: Chapter 5. Air Pollution Meteorology
1Chapter 5. Air Pollution Meteorology
2Outline
- Introduction
- Solar Radiation
- Atmospheric Pressure
- Lapse rate Potential Temperature
- Atmospheric Stability
- Coriolis Force Gravitational Force
- Pressure Gradient Force
- Overall Atmospheric Motion
- Equations of Motion
- Wind Speed Profile
3Introduction (1/2)
- Air pollutant cycle
- Emission
- Transport, diffusion, and transformation
- Deposition
- Re-insertion
- In large urban areas, there are several
concentrated pollutant sources - All sources contribute to pollution at any
specific site - Determined by mainly meteorological conditions
- Dispersion patterns must be established
- Need for mathematical models and meteorological
input data for models
4Introduction (2/2)
- Three dominant dispersion mechanisms
- General mean air motion that transport pollutants
downwind - Turbulent velocity fluctuations that disperse
pollutants in all directions - Diffusion due to concentration gradients
- This chapter is devoted to meteorological
fundamentals for air pollution modelling
5Solar Radiation (1/6)
- Solar constant ? 8.16 J/cm2.min
- 0.4-0.8 µ ? visible range, maximum intensity
Ref http//www.globalwarmingart.com/images/4/4c/S
olar_Spectrum.png
6Solar Radiation (2/6)
- Distribution of solar energy on earth
Ref OpenLearn Web Site,
http//openlearn.open.ac.uk/file.php/1697/t206b1c0
1f26.jpg
7Solar Radiation (3/6)
- At right angle on June, 21 ? Tropic of cancer
- At right angle on December, 21 ? Tropic of
capricorn - At right angle on March, 21 and september, 21 ?
Equator
http//upload.wikimedia.org/wikipedia/commons/8/84
/Earth-lighting-equinox_EN.png
8Solar Radiation (4/6)
- Example What is the Suns angle over Istanbul on
June, 21? Note that Istanbul is located on 40 N
latitude. - Solution Sunlight reaches Tropic of Cancer (23
27') at right angle on June, 21. -
- Where
- ? Suns angle at the given latitude
- L2 Latitude of given region
- L1 Latitude of region where sunlight reaches
surface at right angle
9Solar Radiation (5/6)
- Example What is the Suns angle over a city
located on 39 N latitude when the sunlight
reaches surface at right angle on 21 S latitude?
- Solution
-
10Solar Radiation (6/6)
- Homework (due 18.04.2008)
- Make a brief research on Stefan-Boltzman Law and
write a one page report for your research. - Comment on what would happen if earths
inclination were 24 instead of 2327'. - What determines the seasons? Why some regions of
earth get warmer than other regions. - Calculate the sunlight angle over Istanbul
- on March, 21
- on June, 21
- on September, 21
- on December, 21
11Atmospheric Pressure (1/4)
- Force on earth surface due to the weight of the
atmosphere - Defined as force exerted per unit surface area
- Units of measurement ? Pascal (Pa), atmospheric
pressure unit (apu, atm), newtons per
meter-squared (N/m2), water column (m H2O), etc. - 1 atm 101325 Pa
- 1 atm 10.33 m H2O
- 1 atm 760 mm Hg
- 1 Pa 1 N/m2
- Atmospheric pressure at sea level is 1 atm
12Atmospheric Pressure (2/4)
- Consider a stationary air parcel as shown
- Force balance (assuming no horizontal pressure
gradient)
13Atmospheric Pressure (3/4)
- Integrating from h z0 to h z produces
14Atmospheric Pressure (4/4)
- Homework (due 18.04.2008)
- Make a research about pressure measurement
devices and prepare a one-page report for your
research. Give brief explanations for each type. - Calculate the atmospheric pressure on top of
Everest if it is 1013 mb at sea level.
15Lapse Rate Potential Temperature (1/5)
- Adiabatic ? no heat exchange with surroundings
- Consider an air parcel moving upward so rapidly
that it experiences no heat exchange with
surrounding atmosphere - Enthalpy change
- where
- H1 initial enthalpy of air parcel
- H2 final enthalpy of air parcel
- U1 initial internal energy
- U2 final internal energy
- V1 initial volume
- V2 final volume
16Lapse Rate Potential Temperature (2/5)
- By enthalpys definition
- In infinitesimal expression
- Internal energy substitution
- By internal energy definition
- Enthalpy change is a function of only temperature
when pressure is constant - Substituting differential pressure as follows
- Since the process is adiabatic, no heat exchange
occurs
17Lapse Rate Potential Temperature (3/5)
- This approximation assumed there is no phase
change in the air parcel - called Dry Adiabatic Lapse Rate (DALR)
- If any phase change takes place during the
motion, the temperature change will be far more
different from DALR - Called Saturated (Wet) Adiabatic Lapse Rate
(SALR, WALR) - Variable, must be calculated for each case
- Also significant in some cases this course does
not focus on it - For standardization purposes, Standard Lapse Rate
(SLR), also known as Normal Lapse Rate (NLR), has
been defined - On average, in middle latitude, temperature
changes from 1C to -56.7C - SLR -0.66C/100 m
18Lapse Rate Potential Temperature (4/5)
- Lapse rate measurements are taken by a device
called Radiosonde - Results of measurements are plotted to obtain
Environmental Lapse Rate (ELR) - ELR is real atmospheric lapse rate
- Another significant concept is Potential
Temperature - Defined as possible ground level temperature of
an air parcel at a given altitude
where ? Tp potential temperature of air
parcel T Temperature of air parcel H Height
of air parcel from ground DALR Dry adiabatic
lapse rate
19Lapse Rate Potential Temperature (5/5)
- Homework (due 18.04.2008)
- Calculate potential temperature for given data
- Calculate the atmospheric temperature at 800 m
from the ground if the atmosphere shows adiabatic
characteristic and the ground level temperature
is 12C.
Height, m Temperature, C
350 8
750 2
1200 14
20Atmospheric Stability (1/8)
- If ELR lt DALR Then
- Superadiabatic meaning unstable
- ElseIf ELR DALR Then
- Neutral
- ElseIf DALR lt ELR lt 0 Then
- Subadiabatic meaning stable (weakly stable)
- ElseIf DALR lt 0 lt ELR Then
- Inversion meaning strongly stable
- EndIf
21Atmospheric Stability (2/8)
22Atmospheric Stability (3/8)
23Atmospheric Stability (4/8)
24Atmospheric Stability (5/8)
25Atmospheric Stability (6/8)
- If d?/dz lt 0 Then
- Superadiabatic
- ElseIf d?/dz 0 Then
- Neutral
- ElseIf d?/dz gt 0 Then
- Subadiabatic
- EndIf
26Atmospheric Stability (7/8)
- Example Calculate vertical temperature gradient
and comment on atmospheric stability condition if
the atmospheric temperature at 835 m is 12 C
when the ground temperature is 25 C. - Solution
- The atmosphere is said to be unstable since ELR lt
DALR
27Atmospheric Stability (8/8)
- Homework (due 25.04.2008)
- Following measurements are taken over Istanbul at
different times. Determine atmospheric stability
condition for each case. - Briefly explain stable air, unstable air, neutral
air and inversion. - Make a brief research about the role of
atmospheric stability in dispersion of pollutants
in the atmosphere and prepare a-one-page report
for your research. - What is conditional stability? Explain.
Height, m Temperature, C Temperature, C Temperature, C Temperature, C
Height, m Case 1 Case 2 Case 3 Case 4
0 14 22 17 4
1000 8 8 7 6
28Coriolis Force
- The Coriolis effect is an apparent deflection of
moving objects from a straight path when they are
viewed from a rotating frame of reference.
Coriolis effect is caused by the Coriolis force,
which appears in the equation of motion of an
object in a rotating frame of reference.
(Wikipedia Web Site, http//en.wikipedia.org/wiki/
Coriolis_Force)
29Gravitational Force (1/3)
- The force exerted by the earth on an object in
earths attraction range - Caused by attraction forces between two masses
- m1 being the mass of earth (M) and m2 is that of
an object near earth surface
FA attraction force ? 6.66810-11
Nm2/kg2 m1,m2 objects masses r distance bw
masses
30Gravitational Force (2/3)
- Example Determine the acceleration of an object
near the Eraths surface due to gravitational
attraction force - Solution
31Gravitational Force (3/3)
- Homework (due 25.04.2008)
- Determine the acceleration of an object near the
Martian surface due to gravitational attraction
force - Determine the acceleration of an object near the
Moons surface due to gravitational attraction
force
32Pressure Gradient Force
- Consider an air parcel accelerating in a
horizontal direction - In three dimensional representation,
33Overall Atmospheric Motion (1/7)
- Consider an air parsel accelerating around the
Earth - Overall acceleration
34Overall Atmospheric Motion (2/7)
- Neglecting vertical terms and re-arranging, we get
u velocity of atmospheric motion in east-west
direction v velocity of atmospheric motion in
north-south direction O rotational speed of
earth 7.2910-5 r/s F latitude on which the
motion occurs
35Overall Atmospheric Motion (3/7)
- Example Briefly explain the mechanisms that
forced radioactive pollutants towards Turkeys
coasts after Chernobyl. Tell about the
meteorological conditions then. Show the pressure
centers and wind patterns on the day of accident
and two day after the accident on a brief map.
Consider the aspects of geostrophic winds.
36Overall Atmospheric Motion (4/7)
37Overall Atmospheric Motion (5/7)
- Example Isobars are shown in the figure below,
for 40 latitude in the Northern Hemisphere, at
an altitude of 5600 meters. Determine the
geostrophic wind speed in km/hour - Temperature at 5600 m -28C
- Coriolis force 2 ? V sin ß
- ? 7.3 x 10-5 radians/s ß Latitude degrees
V geostrophic wind speed - 1 mb 100 N/m3
38Overall Atmospheric Motion (6/7)
- ExampleSuppose a nuclear accident occurs at a
place of 3,000 km west of Istanbul. Radioactive
pollutants are pumped above the planetary
boundary layer (PBL) with the power of explosion.
On the day of nuclear accident, the radiosonde
data taken at different places of Europe shows
that atmospheric pressure is decreasing towards
north at a rate of 0.0015 N/m3 and this pattern
is valid for the whole Europe. Will the
radioactivity affect Istanbul? If yes, when? Note
that Istanbul is located on 40 northern latitude
and worlds angular speed of rotation is 7.3
10-5 radians/sec. You may assume the density of
air at the level where geostrophic wind equations
apply as 0.70 kg/m3.
39Overall Atmospheric Motion (7/7)
40Equations of Motion (1/3)
- Eularian Approach
- The observer stays stationary and observes the
change in the value of a function f
(concentration, atmospheric parameters, etc.) - The coordinate system (reference frame) is
stationary - The objective is moving
- Lagregian Approach
- The observer moves with the moving objective and
observes the change in the value of a function f - The coordinate system is moving with the
objective at the same speed and direction
41Equations of Motion (2/3)
- Lagregian Approach (contd)
42Equations of Motion (3/3)
- Examples will be given later
43Wind Speed Profile (1/2)
- Due to friction near surface, wind speed
increases with height exponentially - Wind speed is measured by a device called
anemometer - 10 m should be chosen for anemometer height
Stability Class P
A 0.15
B 0.15
C 0.20
D 0.25
E 0.40
F 0.60
44Wind Speed Profile (2/2)
- Homework (due 25.08.2008)
- Calculate wind speeds for Class B stability at
20, 30, 50, 100, 200, and 500 m if it is 1.2
m/sec. Plot the results. - Comment on how the wind speed would change with
altitude if the stability class were Class E.