BAAO 2022, Теория — Задача 2. Stellar Structure

British Astronomy and Astrophysics Olympiad 2021-2022 — Astronomy & Astrophysics Competition Paper · 24 януари 2022 г. · 35 т.

Указания

This question paper must not be photographed or taken out of the exam room

Time: 3 hours (∼50\sim 50 minutes for Q1, ∼65\sim 65 minutes for Q2 and ∼65\sim 65 minutes for Q3).

Questions: All three questions should be attempted. Each question contains independent parts so that later parts can be attempted even if earlier parts are incomplete.

Solutions: Answers and calculations are to be written on loose paper. Students should ensure their name and school is clearly written on the first answer sheet and that all pages are numbered. EACH QUESTION ANSWERED must be started on a new page. A standard formula booklet with standard physical constants may be used if desired.

Instructions: To accommodate students sitting the paper at different times, please do not discuss any aspect of the paper on the internet until 8 am Saturday 29th January.

Clarity: Solutions must be written legibly, in black pen, and working down the page. Scribble will not be marked and overall clarity is an important aspect of this exam.

Eligibility: The International Olympiad will be held in August 2022; all sixth form students are eligible to participate.

Calculators: Any standard calculator may be used, but calculators cannot be programmable and must not have symbolic algebra capability.

Training Dates and the IOAA

Training Dates and the IOAA (Kyiv, Ukraine, 12th - 22nd August 2022)

The team will be selected from students taking this paper. The best students that are eligible to represent the UK at the IOAA will be invited to attend the Training Camp to be held in Oxford from Saturday 9th to Wednesday 13th April 2022. Astronomy material will be covered; problem solving skills and observational skills (telescope and naked eye observations) will be developed. At the Training Camp a Data Analysis exam along with a Round 3 theory paper will be sat. A team of five students (plus one reserve) will be selected for further training, including additional training camps in the summer.

Important Constants
ConstantSymbolValue
Speed of lightcc3.00×108 m s−13.00 \times 10^{8}\ \mathrm{m\,s^{-1}}
Earth’s rotation period1 day24 hours
Earth’s orbital period1 year365.25 days
parsecpc3.09×1016 m3.09 \times 10^{16}\ \mathrm{m}
Astronomical Unitau1.50×1011 m1.50 \times 10^{11}\ \mathrm{m}
Radius of the SunR⊙R_{\odot}6.96×108 m6.96 \times 10^{8}\ \mathrm{m}
Radius of the EarthR⊕R_{\oplus}6.37×106 m6.37 \times 10^{6}\ \mathrm{m}
Mass of the SunM⊙M_{\odot}1.99×1030 kg1.99 \times 10^{30}\ \mathrm{kg}
Mass of the EarthM⊕M_{\oplus}5.97×1024 kg5.97 \times 10^{24}\ \mathrm{kg}
Luminosity of the SunL⊙L_{\odot}3.85×1026 W3.85 \times 10^{26}\ \mathrm{W}
Stephan-Boltzmann constantσ\sigma5.67×10−8 J m−2 K−45.67 \times 10^{-8}\ \mathrm{J\ m^{-2}\ K^{-4}}
Gravitational constantGG6.67×10−11 m3 kg−1 s−26.67 \times 10^{-11}\ \mathrm{m^{3}\ kg^{-1}\ s^{-2}}
Boltzmann constantkBk_{\mathrm{B}}1.38×10−23 J K−11.38 \times 10^{-23}\ \mathrm{J\ K^{-1}}
Permittivity of free spaceε0\varepsilon_08.85×10−12 F m−18.85 \times 10^{-12}\ \mathrm{F\ m^{-1}}
Permeability of free spaceμ0\mu_04π×10−7 H m−14\pi \times 10^{-7}\ \mathrm{H\ m^{-1}}
Planck’s constanthh6.63×10−34 J s6.63 \times 10^{-34}\ \mathrm{J\ s}
Elementary chargeee1.60×10−19 C1.60 \times 10^{-19}\ \mathrm{C}
Proton rest massmpm_{\mathrm{p}}1.67×10−27 kg1.67 \times 10^{-27}\ \mathrm{kg}
Electron rest massmem_{\mathrm{e}}9.11×10−31 kg9.11 \times 10^{-31}\ \mathrm{kg}
Wien’s displacement lawλmaxT\lambda_{\mathrm{max}}T2.90×10−3 m K2.90 \times 10^{-3}\ \mathrm{m\ K}
Avagadro’s constantNAN_A6.02×1023 mol−16.02 \times 10^{23}\ \mathrm{mol^{-1}}

Basic calculus formulae:

Chain ruleddxf(g(x))=f′(g(x))g′(x)\dfrac{\mathrm{d}}{\mathrm{d}x}f(g(x)) = f'(g(x))g'(x)
Product ruleddx(uv)=dudxv+udvdx\dfrac{\mathrm{d}}{\mathrm{d}x}(uv) = \dfrac{\mathrm{d}u}{\mathrm{d}x}v + u\dfrac{\mathrm{d}v}{\mathrm{d}x}
Quotient ruleddx(uv)=dudxv−udvdxv2\dfrac{\mathrm{d}}{\mathrm{d}x}\left(\dfrac{u}{v}\right) = \dfrac{\frac{\mathrm{d}u}{\mathrm{d}x}v - u\frac{\mathrm{d}v}{\mathrm{d}x}}{v^2}
Integration by parts∫udvdx dx=uv−∫vdudx dx\displaystyle\int u\frac{\mathrm{d}v}{\mathrm{d}x}\,\mathrm{d}x = uv - \int v\frac{\mathrm{d}u}{\mathrm{d}x}\,\mathrm{d}x
Standard integral∫1x dx=ln⁡∣x∣+C\displaystyle\int \frac{1}{x}\,\mathrm{d}x = \ln\vert x\vert + C
Important Formulae

You might find the diagram of an elliptical orbit below useful in solving some of the questions: (the diagram is attached to Qu 3 as a figure)

Elements of an elliptic orbit:

a=OA (=OP)a = \mathbf{OA}\ (= \mathbf{OP})semi-major axis
b=OB (=OC)b = \mathbf{OB}\ (= \mathbf{OC})semi-minor axis
e=1−b2a2e = \sqrt{1 - \frac{b^2}{a^2}}eccentricity
F\mathbf{F}focus
PF=a(1−e)\mathbf{PF} = a(1 - e)periapsis distance (shortest distance from F\mathbf{F})
AF=a(1+e)\mathbf{AF} = a(1 + e)apoapsis distance (longest distance from F\mathbf{F})

Kepler’s Third Law: For an elliptical orbit, the square of the period, TT, of an object about the focus is proportional to the cube of the semi-major axis, aa (as defined above), such that

T2=4π2GMa3 ,T^2 = \frac{4\pi^2}{GM}a^3\ ,

where MM is the total mass of the system (typically dominated by the central object) and GG is the universal gravitational constant.

Vis-Viva Equation: For an elliptical orbit, the speed vv of an object at a distance rr from the focus is related to the semi-major axis, aa, total mass of the system, MM, and universal gravitational constant, GG, (as defined above), such that

v2=GM(2r−1a) .v^2 = GM\left(\frac{2}{r} - \frac{1}{a}\right)\ .

Magnitudes: The apparent magnitudes of two objects, m1m_1 and m0m_0, are related to their apparent brightnesses, b1b_1 and b0b_0, via the formula

b1b0=10−0.4(m1−m0) .\frac{b_1}{b_0} = 10^{-0.4(m_1 - m_0)}\ .

The absolute magnitude of an object, M\mathcal{M}, is the same as its apparent magnitude when viewed from 10 pc, hence the relationship between apparent and absolute magnitude and distance is

m−M=5log⁡(d10) ,m - \mathcal{M} = 5\log\left(\frac{d}{10}\right)\ ,

where dd is measured in parsecs.

Note for markers

BAAO 2021/22 Solutions and Marking Guidelines

Note for markers:

  • Answers to two or three significant figures are generally acceptable. The solution may give more in order to make the calculation clear. Units should be present on final answers when appropriate.
  • There are multiple ways to solve some of the questions; please accept all good solutions that arrive at the correct answer. Students getting the answer in a box will get all the marks available for that calculation / part of the question (as indicated in red), so long as there are no unphysical / nonsensical steps or assumptions made (students may not explicitly calculate the intermediate stages and should not be penalised for this so long as their argument is clear).

Условие

The Sun is our closest star so it is arguably the most studied. Results from detailed observations of how sound waves propagate through the plasma of the Sun allow us to get a sense of the general structure of the Sun, with an upper layer of convecting plasma (leading to the ‘bubbling’ we see with granulation on the surface) and radiative heat transfer below, including a central core region where the pressure and temperature are large enough for nuclear fusion to occur (see Figure 3).

Left: cut-away drawing of the Sun showing the Thermonuclear energy core, the Radiative zone and the Convective zone, with a radial scale 0.2, 0.4, 0.6, 0.8 and circular convection cells in the outer layer. Right: graph titled 'Mass and Luminosity as a function of Radius' with fraction from 0.0 to 1.0 against Radius (r/R) from 0.0 to 1.0; the Luminosity Fraction (dashed purple) rises steeply to 1 by about r/R = 0.25, the Mass Fraction (solid orange) rises more gradually to 1 by about r/R = 0.8.
Figure 3: Left: The general structure of the Sun, with a core in which all the nuclear reactions take place, and convective cells in an outer layer. Credit: Dmitri Pogosyan / University of Alberta. Right: The fraction of the Sun’s mass and the contribution to the Sun’s luminosity as a function of solar radius as determined from detailed computer simulations. Essentially all of the nuclear reactions creating the photons for the Sun’s luminosity take place in a core with a radius of 0.20 R⊙0.20\,R_{\odot} and a mass of 0.35 M⊙0.35\,M_{\odot}. Credit: Kevin France / University of Colorado.

Estimating the conditions in the cores of stars is an important aspect of constructing stellar models. This question explores some of the equations governing stellar structure and estimates the central temperature and pressure of the Sun.

a. (7 т.)

Let rr denote distance from the centre of a star. We define the variables ρ(r)\rho(r), p(r)p(r) and T(r)T(r) to be the density, pressure and temperature at radius rr respectively, and m(r)m(r) to be the mass enclosed within radius rr. We will now try and derive an estimate for the pressure at the centre of the Sun.

(i) By considering forces on a box of height dr\mathrm{d}r at radius rr, show that

dpdr=−ρGmr2 .\frac{\mathrm{d}p}{\mathrm{d}r} = -\rho\frac{Gm}{r^2}\ .

[This is known as the equation of hydrostatic equilibrium.] [2 т.]

(ii) We can get a good estimate of the central pressure if we use mm as our independent variable rather than rr. Derive an expression for dmdr\dfrac{\mathrm{d}m}{\mathrm{d}r} in terms of rr and ρ\rho, and hence express dpdm\dfrac{\mathrm{d}p}{\mathrm{d}m} in terms of mm and rr. [2 т.]

(iii) Assuming that the pressure at the surface, psp_s, is negligible compared to the pressure at the centre of the Sun, pcp_c, the edge of the core is at r=0.20 R⊙r = 0.20\,R_{\odot} and encloses a mass of m=0.35 M⊙m = 0.35\,M_{\odot}, and that dpdm\dfrac{\mathrm{d}p}{\mathrm{d}m} is constant throughout the star and equal to the value at the edge of the core, calculate a value for pcp_c. [3 т.]

b. (7 т.)

The Sun is composed predominantly of ionized hydrogen and helium, with approximate mass fractions X=0.70X = 0.70 and Y=0.30Y = 0.30 respectively (taken to be constant throughout the Sun). These ionized nuclei and electrons may be treated as an ideal monatomic gas, obeying the equation of state

pV=NkBT ,pV = Nk_BT\ ,

where NN is the number of particles contained within volume VV and kBk_B is the Boltzmann constant. They also have an average kinetic energy per particle

EK=32kBT .E_K = \frac{3}{2}k_BT\ .
Diagram of the proton-proton chain: in each of two identical rows, two 1H protons fuse into 2H with emission of a positron and a neutrino ν; 2H plus a 1H proton gives 3He with a gamma ray γ; the two 3He nuclei then combine into 4He, releasing two 1H protons. Legend: Proton (red), Neutron (grey), Positron (white), γ Gamma Ray, ν Neutrino.
Figure 4: An overview of the all the steps in the most common form of the p-p chain, turning four protons into one helium-4 nucleus plus some light particles and photons. Credit: Wikipedia.

(i) Show that the kinetic energy per unit mass of the solar plasma is given by:

u=32kBTmp(2X+34Y) ,u = \frac{3}{2}\frac{k_BT}{m_p}\left(2X + \frac{3}{4}Y\right)\ ,

where mpm_p is the mass of a proton (treated to be the same as the mass of a neutron). [4 т.]

(ii) The Virial Theorem states that for a stable, gravitationally bound system of particles the total kinetic energy in the system, EKE_K and the total gravitational potential energy in the system, EGE_G, are related as

EK=−12EG .E_K = -\frac{1}{2}E_G\ .

In the context of the plasma in the Sun, this becomes

∫0M⊙u dm=−12∫0M⊙−Gmr dm .\int_0^{M_{\odot}} u\,\mathrm{d}m = -\frac{1}{2}\int_0^{M_{\odot}} -\frac{Gm}{r}\,\mathrm{d}m\ .

Using the Virial Theorem, and given EG≈GM⊙2/R⊙E_G \approx G{M_{\odot}}^2/R_{\odot}, estimate the Sun’s mean temperature

⟨T⊙⟩=1M⊙∫0M⊙T dm .\langle T_{\odot}\rangle = \frac{1}{M_{\odot}}\int_0^{M_{\odot}} T\,\mathrm{d}m\ .

[This is our initial lower bound for the central temperature] [3 т.]

The primary nuclear fusion pathway responsible for much of the Sun’s luminous output is called the proton-proton chain (p-p chain). All of the most common steps are shown in Figure 4.

The net reaction of the p-p chain is

4 11H→24He+2e++2νe+2γ .4\,{}^{1}_{1}\mathrm{H} \rightarrow {}^{4}_{2}\mathrm{He} + 2e^{+} + 2\nu_e + 2\gamma\ .

The rate-limiting step is the first one (11H+11H^{1}_{1}\mathrm{H} + {}^{1}_{1}\mathrm{H}) as the probability of interaction is so low, since it requires the decay of a proton into a neutron and so involves the weak nuclear force.

Nuclear physics allow us to calculate the reaction rate coefficient, RR, energy produced per reaction, QQ, and hence the energy generation rate, qq. The reaction rate is related to the number of particles that have enough energy to undergo quantum tunnelling, and the distribution as a function of energy is known as the Gamow peak, with the top of the curve at energy E0E_0. For two nuclei, ZiAiCi^{A_i}_{Z_i}C_i and ZjAjCj^{A_j}_{Z_j}C_j, with mass fractions XiX_i and XjX_j, then to first order and ignoring electron screening,

R=432.5π2hμrmp4πε0ZiZje2S(E0)τ2e−τ ,whereμr=AiAjAi+Aj ,R = \frac{4}{3^{2.5}\pi^2}\frac{h}{\mu_r m_p}\frac{4\pi\varepsilon_0}{Z_iZ_je^2}S(E_0)\tau^2e^{-\tau}\ , \quad \text{where} \quad \mu_r = \frac{A_iA_j}{A_i + A_j}\ ,

and S(E0)S(E_0) measures the probability of interaction at the maximum of the Gamow peak whilst τ\tau is a characteristic width of the Gamow peak,

τ=3E0kBTwhereE0=(bkBT2)2/3givenb=μrmp2πZiZje2hε0 .\tau = \frac{3E_0}{k_BT} \quad \text{where} \quad E_0 = \left(\frac{bk_BT}{2}\right)^{2/3} \quad \text{given} \quad b = \sqrt{\frac{\mu_r m_p}{2}}\frac{\pi Z_iZ_je^2}{h\varepsilon_0}\ .

Here hh is Planck’s constant, ε0\varepsilon_0 is the permittivity of free space and ee is the elementary charge (the charge on a proton). Finally, the energy generation rate per unit mass is

q=ρmp2(11+δij)XiXjAiAjRQ ,q = \frac{\rho}{m_p^2}\left(\frac{1}{1 + \delta_{ij}}\right)\frac{X_iX_j}{A_iA_j}RQ\ ,

where δij\delta_{ij} is the Kronecker delta, so equals 1 when i=ji = j and 0 otherwise.

Evaluating the fundamental constants and defining T6≡T106 KT_6 \equiv \dfrac{T}{10^6\ \mathrm{K}} gives

τ=42.59[Zi2Zj2μrT6−1]1/3 ,\tau = 42.59\left[Z_i^2Z_j^2\mu_rT_6^{-1}\right]^{1/3}\ ,

whilst for the proton-proton interaction Q=13.366Q = 13.366 MeV (half the overall energy of the p-p chain), Zi=Zj=Ai=Aj=δij=1Z_i = Z_j = A_i = A_j = \delta_{ij} = 1, and S(E0)S(E_0) is 4.01×10−504.01 \times 10^{-50} keV m2^2 (Adelberger et al. 2011), so

R=6.55×10−43 T6−2/3e−33.80T6−1/3 m3 s−1andq=0.251ρX2T6−2/3e−33.80T6−1/3 W kg−1.R = 6.55 \times 10^{-43}\,T_6^{-2/3}e^{-33.80T_6^{-1/3}}\ \mathrm{m^3\,s^{-1}} \quad \text{and} \quad q = 0.251\rho X^2T_6^{-2/3}e^{-33.80T_6^{-1/3}}\ \mathrm{W\,kg^{-1}}.

c. (21 т.)

Considering the evaluated equations for τ\tau, RR, and qq we can use this with the measured luminosity of the Sun to get a new estimate for the central temperature.

(i) Considering the simplified equation for qq and assuming that the core has a mass of 0.35 M⊙0.35\,M_{\odot}, throughout which TT and ρ\rho are constant, and that the Sun’s luminosity is equal to the power produced by the p-p chain fusion processes occurring within its core, estimate the central temperature. [Hint: you are also given that u=32pcρcu = \dfrac{3}{2}\dfrac{p_c}{\rho_c} where ρc\rho_c is the central density, and you may need to use a numerical method with ⟨T⊙⟩\langle T_{\odot}\rangle as an initial guess.] [7 т.]

(ii) Using this new central temperature, and considering RR and the central number density of protons, npn_p, estimate the typical amount of time a proton needs to wait to undergo fusion, giving your answer in years.

[This is an estimate for the length of time the Sun spends on the main sequence.] [4 т.]

(iii) Since q∝τ2e−τq \propto \tau^2e^{-\tau} and τ∝T−1/3\tau \propto T^{-1/3}, it can be approximated at a given temperature as q∝Tαq \propto T^{\alpha}, quantifying the sensitivity of the fusion reaction to temperature. By considering d(ln⁡q)d(ln⁡T)\dfrac{\mathrm{d}(\ln q)}{\mathrm{d}(\ln T)} give an expression for α\alpha as a function of τ\tau and calculate it at your central temperature. [6 т.]

(iv) The carbon-nitrogen-oxygen (CNO) cycle is an alternative pathway that becomes important at higher temperatures, where heavier elements catalyse the process of turning hydrogen into helium. There the rate limiting step is between 714N^{14}_{7}\mathrm{N} and 11H^{1}_{1}\mathrm{H}. Compare the temperature dependence of the CNO cycle to the p-p chain at the Sun’s central temperature. [4 т.]

Отговори

Решение

END OF PAPER

END OF PAPER

Questions proposed by:
Dr Alex Calverley (Royal Grammar School, Guildford)
Josh Brown (University of Cambridge)


Оригинал в Архива: BAAO_2022.pdf · официални решения: BAAO_2022_solutions.pdf