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Assignment 4

Due Friday October 18 2024 (on paper at start of class, unless alternate arrangements have been made in advance)

Point values are indicated for each question.

Total points: 30

Question 1

4 points

(Based on Problem 4.3 of the text)

Show the mathematical steps leading from equation (4.17):

g(z)=GME(rE+z)2g(z) = \frac{G M_E}{(r_E + z)^2}

to equation (4.18):

g(z)g0[12(zrE)]g(z) \approx g_0 \left[ 1 - 2\left(\frac{z}{r_E}\right) \right]

where

g0=GMErE2g_0 = \frac{G M_E}{r_E^2}

and rEr_E is the radius of the Earth.

Helpful hints

  1. Start by defining a non-dimensional variable x=zrEx = \frac{z}{r_E}.
  2. Convince yourself that xx is always a small number, so a Taylor series (or power series, same thing) approximation should be useful.
  3. See Appendix C.3 for a refresher on how the series approximation works, for small deviations away from a known reference point.
  4. Rewrite equation (4.17) in terms of xx rather than zz. Do this by substituting z=rE xz = r_E~x into the equation and simplifying.
  5. Use the first-order power series approximation for g(x)g(x) about the reference point x=0x=0.
  6. Show all the steps that lead to equation (4.18)

Question 2

5 points

(Based on Problem 4.5 of the text)

a) (2 points) Show that for the constant density atmosphere, the top of the atmosphere must occur at a height HH above the surface, where

H=RdT0gH = \frac{R_d T_0}{g}

where T0T_0 is the surface temperature.

b) (2 points) What is the temperature at the top of this atmosphere, i.e. T(H)T(H)?

c) (1 point) Based on your results above, comment on whether you think a truly constant density atmosphere could actually exist.

Helpful hints

  1. For constant density ρ0\rho_0, the relationship between pressure and height is given by equation (4.33).
  2. The pressure at the top of the atmosphere must be zero.
  3. Surface pressure and surface temperature are related (as always) through the ideal gas law.
  4. The derivation in section 4.2.1 shows that for a constant-density atmosphere, there is a constant lapse rate g/Rdg/R_d. Use this to find T(H)T(H).

Question 3

12 points

(Based on Problem 4.6 of the text)

a) (3 points) Use the equation for p(z)p(z) for a constant density atmosphere to calculate the approximate height of the 1000, 850, and 500 hPa levels, assuming that the density thoughout the troposphere is the same as that at the surface (computed from T0=15T_0 = 15ºC and p0=1013.2p_0 = 1013.2 hPa).

b) (3 points) Repeat your calculation using the somewhat more accurate expression for p(z)p(z) in an isothermal atmosphere, assuming that the temperature of the entire atmosphere equals T0T_0 as given above.

c) (3 points) Finally, repeat your calculation using the most accurate expression for p(z)p(z), which in this case is the one for a constant lapse rate atmosphere. Assume a lapse rate of Γ=6.5\Gamma = 6.5 K km-1.

d) (3 points) Present your results from parts a-c in a well-formatted and labeled table with data in three rows and five columns. Rows should correspond to the three pressure levels. In the first three columns, report the heights you calculated for the three different model atmospheres. In the final two columns, report the errors (approximate minus true value) for the constant density and isothermal atmospheres. Take your result from part c for the constant lapse rate atmosphere as the “true” value. Report all values to a precision of 1 meter.

Helpful hints

  1. For parts a through c, write down the appropriate equation for p(z)p(z) (one of 4.33, 4.45, and 4.52). Then derive a symbolic solution: Solve the equation for zz so that you have an equation for z(p)z(p) instead of p(z)p(z).
  2. If you’re struggling with how to invert those equations to solve for zz, remember that there is a nice review of the properties of logs and powers in Appendix C.
  3. Once you have the symbolic solution, plug in values to calculate height zz at each of the three pressure levels.
  4. For part d, make sure your table is neat and legible, with units clearly labeled.

Question 4

4 points

(Based on Problem 4.7 of the text)

Assuming a constant lapse rate of 6.5 K km-1 and a surface pressure near 1000 hPa, what value of the 1000-500 hPa thickness should correspond to surface temperatures near freezing?

HINT: To calculate the thickness, you need a formula for the height zz of a pressure surface for an atmosphere with a constant lapse rate. You should be able to reuse a formula you already derived in Question 3.

Question 5

5 points

(Problem 4.8 of the text)

On a certain day, the atmosphere has a temperature T0T_0 of 20°C and a pressure p0p_0 of 1000 hPa at the surface (z0=0z_0 = 0). The lapse rate is Γ0=6\Gamma_0 = 6 K km-1 from the surface to 3 km altitude; Γ1=3\Gamma_1 = 3 K km-1 from 3 km to 6 km altitude. Find the pressure pp at an altitude of 5 km.

HINT: Apply the piecewise linear temperature profile as in section 4.2.4. Start from the surface and work upward.