AOSS 321, Winter 2009 Earth System Dynamics Lecture 3 1/15/2009 Christiane Jablonowski Eric Hetland...
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Transcript of AOSS 321, Winter 2009 Earth System Dynamics Lecture 3 1/15/2009 Christiane Jablonowski Eric Hetland...
AOSS 321, Winter 2009 Earth System Dynamics
Lecture 3 1/15/2009
Christiane Jablonowski Eric Hetland
[email protected] [email protected]
734-763-6238 734-615-3177
Class News• Class web site:
https://ctools.umich.edu/portal• Homework #1 posted today, due on Thursday
(1/22) in class• Our current grader is Kevin Reed (
[email protected])• Office Hours
– Easiest: contact us after the lectures– Prof. Jablonowski, 1541B SRB: Tuesday after
class 12:30-1:30pm, Wednesday 4:30-5:30pm– Prof. Hetland, 2534 C.C. Little, office hour TBA
Today’s lecture
• Ideal gas law for dry air
• Pressure
• Hydrostatic equation
• Scale height
• Geopotential, geopotential height
• Hypsometric equation: Thickness
• Layer-mean temperature
• Mathematical tools
Pressure, temperature, density• Unit 3: Pressure (online resource) http://www.
atmos.washington.edu/2005Q1/101/CD/MAIN3.swf
• Consider a hot air balloon• What is the pressure difference between the inside and outside of the hot air balloon?
• What is the temperature difference between the inside and outside of the balloon?
• What is the density difference?
Pressure, temperature, densityThe ideal gas law
• Pressure is proportional to temperature times density
• Temperature is proportional to the average kinetic energy (mass times velocity squared) of the molecules of a gas
• Density is the mass divided by the volume:
€
ρ =m
V
Ideal gas law
• One form of the ideal gas law is:p V = n R* T
where the number of moles n in mass m (in grams) of a substance is given by
n = m / M
• M is the molecular weight of a substance, e.g. for nitrogen (N2) in the gas phase:
M = 28.0116 g / mol
• p, V, T: pressure, volume and temperature
• R* = 8.3145 J/(K mol): universal gas constant
Another form of the ideal gas law• Another form of the ideal gas law for dry air:
p = ρ Rd T
where Rd is the gas constant for 1 kg of dry air
ρ is the dry air density, units are kg/m3
• Dry air is a mix of different gases, mainly nitrogen
N2, oxygen O2, argon (Ar), carbon dioxide CO2
Mi (g/mol) Volume ratio
N2 28.016 0.7809 21.88
O2 32.000 0.2095 6.704
Ar 39.444 0.0093 0.373
CO2 44.010 0.0003 0.013
Molecular mass of airGasi
€
Σ=28.97 g
mol
Ideal gas law: Conversions• Dalton’s law applies:
– each gas completely occupies the whole volume
– each gas obeys its own pressure law
– total dry air pressure = Σ partial pressures = Σ pi
• Partial pressure of each gas with index i is:
• Using €
piV =mi
M i
R*T = mi
R*
M i
T
⇔ pi =mi
V
R*
M i
T = ρ iRiT with Ri =R*
M i
€
p = pi
i=1
n
∑ , ρ = ρ i
i=1
n
∑ =mi
Vi=1
n
∑ , m = mi
i=1
n
∑
Ideal gas law: Conversions• It follows:
€
p = pi
i=1
n
∑ =1
V
miR*
M i
T =i=1
n
∑mi
i=1
n
∑ ⎧ ⎨ ⎩
⎫ ⎬ ⎭
V
mi
M i
mi
i=1
n
∑ ⎧ ⎨ ⎩
⎫ ⎬ ⎭
R*Ti=1
n
∑
= ρ
mi
M i
mi
i=1
n
∑
⎧
⎨ ⎪ ⎪
⎩ ⎪ ⎪
⎫
⎬ ⎪ ⎪
⎭ ⎪ ⎪
R*T =i=1
n
∑ ρTR*
mi
M ii=1
n
∑
mi
i=1
n
∑
⎧
⎨ ⎪ ⎪
⎩ ⎪ ⎪
⎫
⎬ ⎪ ⎪
⎭ ⎪ ⎪
= ρTR*
Md
= ρTRd
€
=ρ
Conversions• with Md: apparent molecular weight of dry air
• Gas constant for dry air:
€
Md =
mi
i=1
n
∑mi
M ii=1
n
∑= 28.97
g
mol
€
Rd =R*
Md
=8.3145 J mol
28.97 g mol K= 0.287
J
g K
= 287 J
kg K= 287
N m
kg K
Ideal gas law (used in atmospheric dynamics)
• Ideal gas law for dry air:
p = ρ Rd T
• p: pressure in Pa
ρ: density in kg/m3
• Rd: gas constant for 1 kg of dry air Rd = 287.0 J /(K kg)
• T: temperature in K
Hydrostatic Equation: Derivation• Pressure (per 1 m2) at point 1:
• Pressure (per 1 m2) at point 2:
• Compute pressure differencebetween layer 1 and 2
•
• Rearrange:
p2
p1
z2
z11
2z
Column of air withdensity ρ higher z
higher pz = 0m
€
p = p1 − p2 = ρgz1 − ρgz2
= ρgz1 − ρg z1 + Δz( )
= ρgz1 − ρgz1 − ρgΔz = −ρgΔz
€
p1 = ρgz1
€
p2 = ρgz2 = ρg z1 + Δz( ) with
Δz = z2 − z1
€
p = −ρgΔz ⇔
€
p
Δz= −ρg
Hydrostatic equation
• p: pressure in Pa• z: height in m ρ: density in kg/m3
• g: gravitational acceleration of the Earth, approximately constant, g = 9.81 m/s2
€
∂p
∂z= −ρg
Pressure
• Pressure decreases with height in the atmosphere– Why?
• Pressure increases with depth in the ocean– Why?
• Atmosphere exerts a downward force on the underlying surface due to the Earth’s gravitational acceleration
• Downward force (here: the weight force) of a unit volume (1 m3) of air with density ρ is given byF/V = ρ g
Pressure and mass• The atmospheric pressure due to the weight
(per unit area) of the air in an overlying column
• Usually we assume that the gravitational acceleration g is constant: g = g0
• m: vertically integrated mass per unit area of an overlying column of air at height z:€
p(z) = ρz
∞
∫ gdz'= m(z)g0
€
m(z) = ρz
∞
∫ dz'
Surface Pressure ps
• At the surface
• With m:
vertically integrated mass per unit area (!) of an overlying column of air at the surface, units:kg/m2
• We get:
€
ps = ρ0
∞
∫ gdz'
€
m = ρ0
∞
∫ dz'
€
ps = mg0
1st Exercise
• Compute the pressure profile p(z) with respect to the height z for an isothermal (constant) atmosphere
• Assume a flat Earth (no mountains): The surface height is z0 = 0 m
• Assume the surface pressure p0 = p(z0) is known
€
∂p
∂z= −ρg
€
T
Scale Height
• : average (constant) temperature• Scale height of the atmosphere: around 8km• This is the height where the pressure of the
atmosphere is reduced by a factor of 1/e• For isothermal atmosphere with z0 = 0 m (as seen
before):
€
H =Rd T
g
€
T
€
p = p0 exp(−z /H)
2nd Exercise• Compute the pressure profile p(z) with respect
to the height z for an atmosphere whose temperature varies with height like:T = T0 - z
• T0 = T(z0) is the known surface temperature at the surface height z0
is a known, constant vertical temperature gradient (lapse rate) = -∂T/∂z, units K/m
• Assume a flat Earth (no mountains): z0 = 0 m
• Assume the surface pressure p0 = p(z0) is known
• Ideal gas law for dry air:
• Hydrostatic equation
• Define the geopotential:
• Note that
Some definitions
€
∂p
∂z= −ρg
€
p = ρRdT
€
Φ= gdz0
z
∫
€
dΦ
dz= g ⇔ dΦ = gdz
Hypsometric equation: Derivation• Express the hydrostatic equation in terms of the
geopotential:
• The variation of the geopotential with respect to pressure only depends on the temperature
€
∂p
∂z= −ρg
⇔∂p
∂z= −
pg
RdT
⇔ −RdT
pdp = gdz = dΦ
⇔ dΦ = −RdTdp
p= −RdT d ln p( )
Hypsometric equation: Derivation
• Integration in the vertical gives:
• Hypsometric equation:
€
Φ(z2) − Φ(z1) = g(Z2 − Z1) = Rd
T
pdp
p2
p1
∫ = Rd Td ln pp2
p1
∫€
dΦz1
z2
∫ = − RdTd(ln p)p1
p2
∫
⇔ Φ(z2) − Φ(z1) = Rd Td(ln p)p21
p1
∫
Hypsometric equation
• With the definition of the geopotential height:
• the hypsometric equation becomes:
• ZT: Thickness of an atmospheric layer (in m) between the pressure surfaces p2 and p1€
ZT = (Z2 − Z1) =Rd
g
T
pdp
p2
p1
∫ =Rd
gTd ln p
p2
p1
∫€
Z =Φ(z)
g(with constant g)
Hypsometric equation for isothermal atmospheres
• If the atmosphere is isothermal with T=T0 the hypsometric equation becomes:
• with scale height H = RdT0/g, g = 9.81m s-2
• We see: the thickness of a layer bounded by two isobaric pressure surfaces is proportional to the mean temperature (here constant T0) of the layer
€
ZT =RdT0
gd ln p
p2
p1
∫ = H lnp1
p2
⎛
⎝ ⎜
⎞
⎠ ⎟
Layer mean temperature
• In an isothermal atmosphere with T0 the layer mean temperature is
• More general definition of the layer mean temperature (for non-isothermal atmospheres):
€
T = T0
€
T =
Td ln pp2
p1
∫
d ln pp2
p1
∫
Examples
• Unit 3 (online resource), frame 20: Dependence on the 800 hPa height on temperaturehttp://www.atmos.washington.edu/2005Q1/101/CD/MAIN3.swf
• Assess the height of the800 hPa surface on a cold and hot day:
Source: Dale Durran,University of Washington
Hot air balloon revisited
• Pressure is the same at the top of the two columns. hotter (red) column is taller than cold (blue) column
• Pressure is the same inside and outside at the bottom of the balloon
• How does the pressure at point O compare to the pressure at point I ?
O I
Example: Weather maps• 500 hPa geopotential height map• Blue: isolines that connect equal geopotential
height values (in dm= 10 m)
Weather maps:http://www.rap.ucar.edu/weather/model/
564
576
552
Real weather situations:850 hPa temperature and geopot. thickness
warm air,high geopotentialheight values
cold air, low geopotentialheightvalues
warm
cold
Mathematical tools: We use• Logarithms and exponential functions• Integrals• Derivatives:
– Partial derivatives– Chain rule, product rule
• Sine, cosine• Vectors and vector calculus• Operators:
– Gradient– Divergence– Vector (cross) product
• Spherical coordinates
Logarithms and exponentials• Natural logarithm, manipulations
– ln (x) for x > 0– ln (x/y) = ln(x) - ln(y)– ln (x*y) = ln(x) + ln (y)– a * ln(x) = ln (xa)– Values: ln(1) = 0, – ln (exp (x)) = x,
• exp (ln(x)) = x• xa * xb = xa+b
• (xa)b = xa*b
• (x y)a = xa ya
€
limx →∞
ln x( ) = ∞,limx →0
ln x( ) = −∞€
Integrals• Integrals without limits, a ≠0 is a constant:
€
1
x∫ dx = ln x
€
1
ax∫ dx =
1
aln ax( )
€
exp(x)∫ dx = exp x( )
€
exp(ax)∫ dx =1
aexp ax( )
€
ax n∫ dx =a
n +1( )x n +1 (for n ≠ -1)
€
sin(ax)∫ dx = −1
acos(ax)
€
cos(ax)∫ dx =1
asin(ax)
Derivatives, partial derivatives• Derivatives, a ≠0 is a constant:
• Partial derivatives: treat the variables that arenot differentiated as constants, e.g. f(x,y,z)=xyz
€
d
dxln x =
1
x
€
d
dxexp ax( ) = aexp(ax)
€
d
dxa(x n ) = anx n−1 €
d
dxcos(ax) = −asin(ax)
€
d
dxsin(ax) = acos(ax)
€
∂∂x
(xyz) = yz,∂
∂y(xyz) = xz,
∂
∂z(xyz) = xy
Cartesian Coordinates
xy
z
ij
k
east
north
Local vertical
Velocity vector v = (ui + vj + wk)i: unit vector in x directionj: unit vector in y directonk: unit vector in z direction
Vector notationDefine two vectors, A and B, in a Cartesian coordinate system:
€
A =r A = Axi + Ay j + Azk
A=(Ax,Ay,Az)T is a vector
other symbol: A=(Ax,Ay,Az), also
i, j, k are unit vectors (here in Cartesian coordinates), normalized, orthogonal
€
A = A
€
B =r B = Bxi + By j + Bzk
Vector calculus
Are you comfortable with:• c * A, c is a scalar constant• Magnitude of a vector A: |A|• A + B, A - B• Scalar product of two vectors:• Vector product:• Gradient of a scalar, e.g. T:• Divergence:• Curl:
€
A • B
€
∇• A
€
A × B
€
∇T
€
∇×A
Unit vectors
Unit vectors in Cartesian coordinates
Unit vectors are normalized: |i| = |j| = |k| = 1
i, j, k are orthogonal:
Example: i•i = 1, i•j = 0, i•k = 0
€
i =
1
0
0
⎛
⎝
⎜ ⎜ ⎜
⎞
⎠
⎟ ⎟ ⎟
€
j =
0
1
0
⎛
⎝
⎜ ⎜ ⎜
⎞
⎠
⎟ ⎟ ⎟
€
k =
0
0
1
⎛
⎝
⎜ ⎜ ⎜
⎞
⎠
⎟ ⎟ ⎟
Magnitude and dot product(Cartesian coordinates)
• Magnitude of a vector: |A|
• Scalar (dot) product: A•B = |A| |B| cos() : angle between A and B €
A = Ax2 + Ay
2 + Az2
[ ]
€
A• B = AxBx + AyBy + A zBz
Sum/Subtraction of two vectors(Cartesian coordinates)
• Sum of two vectors: A + B = (Ax+Bx)i +(Ay+By)j +(Az+Bz)k
• Subtraction of two vectors: A - B = (Ax-Bx)i +(Ay-By)j +(Az-Bz)k
Subtraction:AB
Sum:
A
B
-B
Vector (cross) product(Cartesian coordinates)
• Vector product:
• In component form:C = A x B = (AyBz - AzBy)i + (AzBx - AxBz)j + (AxBy - AyBx)k
• The resultant vector C is in the plane that is perpendicular to the plane that contains A and B (direction: right hand rule)
C
A
B
€
rA ×
r B =
i j k
Ax Ay Az
Bx By Bz
€
A × B = A B sinα
determinant
Gradient(Cartesian coordinates)
• Gradient of a scalar, e.g. temperature T:
• Resulting vector quantity, use of partial derivatives€
∇T =
∂
∂x∂
∂y∂
∂z
⎛
⎝
⎜ ⎜ ⎜ ⎜ ⎜ ⎜
⎞
⎠
⎟ ⎟ ⎟ ⎟ ⎟ ⎟
T =
∂T
∂x∂T
∂y∂T
∂z
⎛
⎝
⎜ ⎜ ⎜ ⎜ ⎜ ⎜
⎞
⎠
⎟ ⎟ ⎟ ⎟ ⎟ ⎟
Horizontal temperature gradients
• Horizontal temperature gradient vector:
• Imagine the isotherms (solid lines)are oriented in the E-W direction
• Draw the horizontal temperature gradient vector.
€
∇hT =
∂T
∂x∂T
∂y
⎛
⎝
⎜ ⎜ ⎜
⎞
⎠
⎟ ⎟ ⎟
cold
warm X
y
Horizontal temperature gradients• Solid lines are isotherms
• Compute the components of the
2D temperature gradient vector:
€
∇hT =
∂T
∂x∂T
∂y
⎛
⎝
⎜ ⎜ ⎜
⎞
⎠
⎟ ⎟ ⎟≈
ΔT
ΔxΔT
Δy
⎛
⎝
⎜ ⎜ ⎜
⎞
⎠
⎟ ⎟ ⎟
X
yy=100 km
300 K
280 K
270 K
290 Kx=100 km
Horizontal temperature gradients• How does the situation change below?
• Compute the components of the 2D temperature
gradient vector:
X
yy=100 km
300 K
280 K
270 K
290 K
x=100 km
Horizontal temperature gradients
• Draw the horizontal temperature gradient vector.• Solid lines are isotherms, they are 10 K apart.
cold
warm
X
y
Can you compute the components of the gradient vector?
y=100 km
x=100 km