ch.$3$atmospheric$thermodynamics$ - jackson school of ... · 1− e p + er d pr v " # $ %...
TRANSCRIPT
![Page 1: Ch.$3$Atmospheric$thermodynamics$ - Jackson School of ... · 1− e p + eR d pR v " # $ % & '= p R d T 1− e p (1+ε) " # $ % & ' (eq. 2) where ε= R d R v =0.622 If we insist on](https://reader034.vdocuments.net/reader034/viewer/2022042218/5ec3e66f97890f088570113b/html5/thumbnails/1.jpg)
Ch. 3 Atmospheric thermodynamics
Chapter 3 in the text book References: Thermodynamics of the atmosphere and ocean by Curry and
Webster
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Outline: • Dry gas laws (The text 3.1-‐3.4, p63-‐79) • Moist air (The text, 3.5-‐3.7, p79-‐101)
How do we define dry and moist air?
– Dry air: can include water vapor but does NOT involve water phase change, i.e., condensaSon/freeze, melt/evaporaSon.
– Moist air: air involves water phase change.
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3.1 Dry Gas Laws
• The idea gas law • Virtual temperature • The hydrostaSc equaSon: geopotenSal height and thickness, the scale height,
• The first law of the thermdynamics • AdiabaSc processes and potenSal temperature
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The idea Gas Law:
• The the atmosphere, whether considered individually or as a mixture, follows a state equaSon that describes the relaSonship between air pressure, volume and temperature.
• Various forms of the idea gas law: – PV=mRT
• P: pressure (Pa), V: volume (m3), m: mass (kg), T: absolute temperature (K), R: the gas constant for 1 kg of gas.
– P=ρRT or αP=RT • Where ρ=m/V, air density, α=1/ρ: the specific volume
– PV=nR*T If we let PV=m(kg)RT=(1000m(g)/M)(MR)T=nR*T • Where n=m/M, M: molecular weight of a mole of gas (6.022X1023 molecules), n:
the number of moles in mass m. R*=MR/1000: gas constant for 1 mol of gas, =8.3145 J K-‐1 mol-‐1, or universal gas constant
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The idea Gas Law-‐2:
• Various forms of the idea gas law: – P=nokT for a gas containing no melecules
• k=R*/NA: Boltzmann constant, no: number of moleucles per unit volume, NA: number of molecules per mole.
– Pdαd=RdT for dry air • “ d”: dry air • Molecular weight of dry atmosphere, Md: 28.97~29, • Gas constant for 1 kg of dry atmosphere, Rd=1000xR*/Md
=1000*8.3145/28.97=287.0 J K-‐1kg-‐1.
– evαv=Rv*T for water vapor • ev: vapor pressure, “ v”: water vapor • Water vapor gas constant: Rv=1000xR*/Md=1000*8.3145/18.016 =461.51 J K-‐1kg-‐1.
– Rd/Rv=Mv/Md=18.016/28.97=0.622 QuesSon: can we apply the idea gas law to a mixture of dry air and water vapor?
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The virtual temperature, Tv:
• Atmosphere is a mixture of dry air and water vapor ρ =
md +mv
V= ρd + ρv
dry air and water vapor each follow the idea gas law:pd = ρdRdT and ev = ρvRvTthe total air pressure (dry +vapor), p=pd + e Dalton's law (eq. 1)
ρ=ρd + ρv =p− eRdT
+eRvT
=pRdT
1− ep+eRdpRv
"
#$
%
&'=
pRdT
1− ep
(1+ε)"
#$
%
&' (eq. 2)
where ε= RdRv
= 0.622
If we insist on applying the idea gas law for the mixed dry air and vaporand treat it as if it were dry air:b p=ρRdT', where T' has to be slightly different warmer than T (why?) and substitute eqs. 1 and 2: we would have
p= pRdT
1− ep
(1+ε)"
#$
%
&'RdT' T'= 1
1− ep
(1+ε) T
Tv =T'= 1
1− ep
(1+ε) T defined as the virtual temperature
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The virtual temperature, Tv-‐2:
• What does Tv mean? – The temperature of dry air that has the same air density at
the same pressure as the mixture of dry air and water vapor.
• Why is Tv warmer than T? – Because water vapor has lighter molecular weight (18) than
that of dry air (~29), Tv is higher than T so it’s corresponding dry air density would be lowed to that of the mixture of dry air and water vapor.
• What controls the deviaSon of Tv from T? – The high humidity is, the higher Tv is relaSve to T.
€
Tv = 1
1− ep
(1+ε ) T
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Example:
• Compare Tv for surface air consists of 4% of water vapor to that consists of 1% of water vapor. Assuming that the surface pressure is 1000 hPa and T is 25C.
€
Tv = 1
1− ep
(1−ε) T
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Example:
• Compare Tv for surface air consists of 4% of water vapor to that consists of 1% of water vapor. Assuming that the surface pressure is 1000 hPa and T is 25C.
€
At the surface, p = 1000 hpa, for air with 4% water vapor, e = 0.04X1000 hpa = 40 hPa
Tv =T
1− ep
(1−ε)=
(25+ 273)K
1− 40hpa1000hPa
(1− 0.622)=
298K0.985
= 302.5K = 29.5C
For air with 1% water vapor, e = 0.01X1000 hpa = 10 hPa
Tv =T
1− ep
(1−ε)=
(25+ 273)K
1− 10hpa1000hPa
(1− 0.622)=
298K0.996
= 299.2K = 26.2K
3% of extra water vapor in the atmosphere has the same impact onair density as 3.3K temperature increase for atmosphere with 1% water vapor.
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Exercise:
• Compare Tv between the surface air and air at 500 hPa. In both case, water vapor is 4% of the total air mass. Assuming that the surface pressure is 1000 hPa and T is 25C, and T at 500 hPa is -‐8C.
• Compare the difference between T and Tv at both the surface and 500 hPa. Explain what cause the difference.
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Exercise:
• Compare Tv between the surface air and air at 500 hPa. In both case, water vapor is 4% of the total air mass. Assuming that the surface pressure is 1000 hPa and T is 25C, and T at 500 hPa is -‐8C.
• Compare the difference between T and Tv at both the surface and 500 hPa. Explain what cause the difference.
€
At the surface, p = 1000 hpa, 4% water vapor, e = 40 hPa
Tv =T
1− ep
(1−ε)=
(25+ 273)K1− 0.04(1− 0.622)
=298K0.985
= 302.5K = 29.5C
At 500 hP, T = (-8 + 273)K = 265K, 4% water vapor, e = 0.04X500 hpa = 20 hPa
Tv =T
1− ep
(1−ε)=
265K1− 0.04(1− 0.622)
=265K0.985
= 269.0K = 26C
The difference between T and Tv is smaller because of lower temperature at 500 hPa.
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• The hydrostaSc equaSon: geopotenSal height and thickness, the scale height,
• The first law of the thermodynamics
• AdiabaSc processes and potenSal temperature
Two physical principles and applica1ons for dry air thermodynamics:
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3.2 The hydrosta/c equa/on
• Air pressures at any given height in the atmosphere is due to gravitaSonal force of the air mass above that height,
• Thus, change of surface pressure at a height is due to change of air mass above that height. – dp(z)=-‐ρgdz or dp/dz=-‐ρg The hydrostaSc equaSon
• It is a good approximaSon for large-‐scale
atmospheric and climate dynamic processes, but not a good approximaSon for fast mesoscale convecSve processes, such as supercell, tornadoes. Why?
€
p(z) = ρ(z)gdzz
∞
∫
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Why cannot we use hydrostaSc equaSon in case of rainfall and thunderstorms?
€
ρ ⋅az = Fz∑
z : vertical direction, az : vertical acceleration, Fz : forces in vertical direction, ρ : air density
ρdwdt
= −gρ − dpdz
− ρa friction
g : gravitational acceleration, p : pressure, a friction : deceleration by friction, w : vertical velocity
Away from convection, dwdt
~ 0, friction of the atmosphere is small, thus a friction ~ 0
Thus − gρ − dpdz
~ 0 1ρdpdz
= - g hydrostatic equation
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3.2.1 Geopoten/al
• The work to against gravity for an rising air mass, or potenSal energy of air at a height z,
• GeopotenSal height:
• Because gravitaSonal acceleraSon decreases with
height, the geometric height does not exactly represent the potenSal energy of the air at high alStude. Thus, we use geopotenSal height to represent the TRUE value of the potenSal energy of the atmosphere at a given height. – In the lower troposphere, gègo, Z=z – In the upper troposphere, Z starts to deviate from z
€
dΦ = gdz = −1ρdp = −αdp = −RT dp
p= RTd ln p
Φ(z) = gdz =0
z∫ − αdp
p(z)
ps∫
€
Z ≡Φ(z)go
= −1go
gdzz
∞
∫g: gravitaSonal acceleraSon at alStude z Go=9.81 m/s2, : global mean g at surface
Table 3.1: Values of the geopotenSal height (Z), and acceleraSon due to gravity (g), at 40◦ laStude for geometric height (z)
z(km) Z(km) g(m s−2) 0 0 9.81 1 1.00 9.80 10 9.99 9.77 100 98.47 9.50 500 463.6 8.43
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3.2.2 Geopoten/al height:
• GeopotenSal height is more commonly used in pressure coordinate, in which it represents the potenSal height of the air at a given pressure level:
• GeopotenSal height at the given pressure level is determined by T of the air from the surface to that level, which in turn determines the height of the pressure level. €
Z ≡Φ(z)go
= −1go
αdp = −1go
RTd ln pp
ps∫p
ps∫
z
Z500 hPa
colder warmer
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3.2.3 Geopoten/al thickness:
• GeopotenSal height difference between the bopom and top of an atmospheric layer:
• QuesSon: What determine the thickness of an atmospheric layer? €
dZ ≡dΦ(z)go
For dry air :
Z2 − Z1 =1go
dΦz1
z2∫ = −1go
RTd ln pp2
p1∫ = RT lnp2
p1
for dry air with vapor :
Z2 − Z1 =1go
dΦz1
z2∫ = −1go
RTvd ln pp2
p1∫ = RTv ln p2
p1Hypsometric equa/on
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Scale height:
• Scale height: the geopotenSal height of the atmospheric layer if it were an isothermal layer. It depends on the temperature and gas constant of the air. It is used as a scaling factor in determining the geopotenSal height of a given pressure level.
€
Z2 − Z1 =Rgo
Tvdppp2
p1∫For an isothermal atmosphere layer, if the virtual effect is neglected
Z2 − Z1 =RTgo
ln p2
p1
= Hn p2
p1
where H ≡RTgo
is the scale height
• Different gases have different scale height for the same T • Scale height increase with T, the isothermal gas column expands verScally with T. • Why use scale height?
• Easy to convert between Z and P • An important characterizaSon of a fluid or gas layer.
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• Scale height of the earth’s atmosphere under current insolaSon:
€
For the earth's atmosphere, Rd = 287.0 J K-1 kg-1, go = 9.81ms−1
H =Rd
goT =
287.0 J K-1 kg-1
9.81ms−1 T = 29.3T m K-1
For T = 255K, the approximate mean T of the atmosphere (Te)H = 7.47 ×103m = 7.47km The earth's atmosphere scale height is about 7.5 km averaged globally
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In class exercise: What would be the scale height of the earth’s atmosphere, • A) if the solar radiaSon were decreased by 1% relaSve to the current solar
radiaSon intensity and lead to an 1k decrease of earth’s effecSve temperature, • B) if the atmosphere consisted 100% water vapor? Use T=255K
Rv=461.51 JK-‐1kg-‐1, • C) if we need to consider the virtual effect of the atmosphere with 1% water vapor
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What would be the scale height of the earth’s atmosphere, • A) if the solar radiaSon were decreased by 1% relaSve to the current solar
radiaSon intensity and lead to an 1k decrease of earth’s effecSve temperature, • B) if the atmosphere consisted 100% water vapor? Use T=255K
Rv=461.51 JK-‐1kg-‐1, • C) if we need to consider the virtual effect of the atmosphere with 1% water vapor
€
a)Te = 254K
H = 29.3X254 m K-1 = 7.44 ×103m = 7.44km The earth' s atmosphere scale height would be 7.44 km averaged globally, about 300 m lower than that of the current climate.b)
Rv = 461.51JK −1kg−1
H =RvTgo
=461.51JK −1kg−1
9.81ms−2 255K = 11,996 m = 12.00 km
c)
H = RdTvgo
=RdT
go 1− ep
(1− 0.622)$
% &
'
( )
=287.0JK −1kg−1 × 255K
9.81ms−2 1− 0.01* (1− 0.622)( )= 7489m = 7.49km
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• Thickness of the atmosphere between two pressure levels:
€
ΔZ = Z2 − Z1 =RTvgo
ln p2
p1
= 29.3Tv ln p2
p1
if we want to consider Tv
Between 1000 hPa to 700 hPa, ΔZ = 29.3Tv ln1000hpa700hPa
=10.45Tv m/K
For Tv = 280K, ΔZ1000-700hPa = 2926mFor Tv = 282K, ΔZ1000-700hPa = 2947m
Warm core system Cold core system
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Summary:
• The atmosphere is governed by ideal gas law, p=ρRT • To simplify the ideal gas law for mixed dry air and water
vapor, we introduce virtual temperature,
• To describe atmospheric layer thickness change with temperature, we introduce geopotenSal height, Z, and scale height, H. Both increase with an increase of T.
€
Tv = 1
1− ep
(1−ε) T
€
Z ≡Φ(z)go
= −1go
αdp = −1go
RTd ln pp
ps∫p
ps∫