Physics 136b: Homework Solutions for Chapter 16 - Supersonic Flow, Assignments of Physics

Solutions to homework problems from chapter 16 of physics 136b, focusing on supersonic flow, including derivations of equations for a steady ideal gas outflow from a spherical gaseous planet, analysis of transonic flow, and the study of a spherical projectile entering earth's atmosphere.

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Physics 136b
Homework associated with Chapter 16, Supersonic Flow
Available Feb 19, 2001
Due, Monday Feb 26
As usual, if any problem is trivial for you, do not do it – simply state that it
is trivial and pick some other problem or make up your own. Contact me
([email protected]) if you have a question or concern about Problems 1 &
2 , which are new. There are only three problems this week.
1. If you place a gaseous (Jupiter-like) planet too close to a star then it will
tend to “evaporate”: A solar wind-like outflow will develop, driven by
the UV flux of the star. This limits the survival time for some of the kinds
of extrasolar planets recently discovered in very short period orbits.
(a) Consider a steady, ideal gas outflow from a spherical gaseous planet.
Show that the relevant set of equations (energy, momentum and
continuity) can be written as:
where u is the radial gas flow, ρ is the gas density, p is the pressure, γ is
the ratio of specific heats, M is the planetary mass (considered to be
almost entirely below the radius of interest) and Γ is the volumetric
heating rate (caused by the UV flux). Steady flow means dM/dt is a
constant (on a dynamical time scale, not necessarily long time scales).
(b) From these equations, derive an equation (of the standard solar wind
or transonic form):
tudr
d(2
1u2+c- 1
c
t
p-r
GM ) = C(r)
udr
du =-t
1
dr
dp -r2
GM
dt
dM =-4rt(r)u(r)r2
(u2-c2)u
1
dr
du =somethin
g
c2/t
cp
pf3

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Physics 136b

Homework associated with Chapter 16, Supersonic Flow Available Feb 19, 2001 Due, Monday Feb 26

As usual, if any problem is trivial for you, do not do it – simply state that it is trivial and pick some other problem or make up your own. Contact me ([email protected]) if you have a question or concern about Problems 1 & 2 , which are new. There are only three problems this week.

  1. If you place a gaseous (Jupiter-like) planet too close to a star then it will tend to “evaporate”: A solar wind-like outflow will develop, driven by the UV flux of the star. This limits the survival time for some of the kinds of extrasolar planets recently discovered in very short period orbits.

(a) Consider a steady, ideal gas outflow from a spherical gaseous planet. Show that the relevant set of equations (energy, momentum and continuity) can be written as:

where u is the radial gas flow, ρ is the gas density, p is the pressure, γ is the ratio of specific heats, M is the planetary mass (considered to be almost entirely below the radius of interest) and Γ is the volumetric heating rate (caused by the UV flux). Steady flow means dM/dt is a constant (on a dynamical time scale, not necessarily long time scales).

(b) From these equations, derive an equation (of the standard solar wind or transonic form):

t u drd^ ( 21 u^2 + (^) c c- 1t^ p^ - GMr^ ) = C ( r )

u dudr^ = - (^) t^1 dpdr^ - r^2

GM

dt

dM (^) = - 4rt ( r ) u ( r ) r^2

( u^2 - c^2 ) (^) u^1 dudr^ = something

c^2 / ct p

from which you should derive the conditions for a transonic flow (the only solution that crosses u < c to u>c as r increases):

where subscript s means the quantity evaluated at the critical (sonic) radius rs (the value of which is implicitly defined by this equation).

(c) From the energy equation and constant mass flux, derive the approximate result

where subscript m refers to the smallest radius that the UV effectively penetrates (called optical depth unity in UV). This result neglects um^2 and pm/ρm relative to GM/rm, which is physically plausible except at very

high fluxes.

(d) At r > rm, we have Γ~ κρFUV where κ is the UV opacity and FUV is the UV flux (this assumes strong efficiency of conversion of UV flux to heating, which is often true). And we have the statement that defines rm:

Deduce that a plausible approximation is

and offer a simple physical interpretation of this result. (“Plausible” means you need to suggest why other terms might be neglected.)

(e) Find the survival time for a 10^30 g body (half Jupiter mass) of radius 1010 cm in a UV flux of 4 x10^5 erg/cm^2 .sec (corresponding to about 0. AU orbital radius). [In reality, these kinds of bodies actually get larger as mass is removed, which means they will eventually flow over the Roche lobe, defined as the region in which the planetary gravity dominates].

cs^2 = us^2 =^ GM 2 rs^ + (c^2 - 1)d^ C (^) t ur n s

dt

dM (^) = 4 r r^2 C ( r ) dr / [ rm

GM rm

rs

# + 4 (c - 1)

5 - 3c rs

GM (^) + 4

c + 1 t u d^ C r n s

]

tl dr ~ rm

3

dt

dM (^) = GM

4 r rm^3 FUV