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We simulate the critical collapse of a spherically symmetric massless scalar field ϕ in polar coordinates,
$ {\rm d} s^{2}=-A(r,t)\rm{e}^{-2\delta(r,t)}\rm{d}t^{2}+\frac{1}{A(r,t)}\rm{d}r^{2}+r^{2}\rm{d}\Omega^2. $
(1) The energy-momentum tensor for the scalar field is
$ T_{\mu\nu}=\phi_{,\mu}\phi_{,\nu}-(1/2)g_{\mu\nu}g^{\alpha\beta}\phi_{,\alpha}\phi_{,\beta} $ . Some components of the Einstein and energy-momentum tensors for ϕ are shown below.$ \begin{array}{*{20}{l}} \begin{split} G^{t}_{t}&=\frac{1}{r^2}(rA_{,r}-1+A),\\ G^{r}_{r}&=-\frac{1}{r^2}(-rA_{,r}+2rA\delta_{,r}+1-A),\\ G^{r}_{t}&=-\frac{1}{r}A_{,t},\\ T^{t}_{t}&=-T^{r}_{r}=-\frac{1}{2}A(P^2+Q^2),\\ T^{r}_{t}&=A\phi_{,r}\phi_{,t}. \end{split} \nonumber \end{array} $
Here,
$ (_{,r}) $ and$ (_{,t}) $ denote partial derivatives with respect to the coordinates r and t, respectively.We define
$ \begin{array}{*{20}{l}} Q(r,t)\equiv\phi_{,r}, \hphantom{dd} P(r,t)\equiv A^{-1}\rm{e}^{\delta}\phi_{,t}, \end{array} $
(2) and set
$ G=1 $ . Then, the equations$ G^{t}_{t}=8\pi T^{t}_{t} $ and$ G^{r}_{t}= 8\pi T^{r}_{t} $ respectively generate$ A_{,r}=\frac{1-A}{r}-4\pi rA(P^{2}+Q^{2}), $
(3) $ \begin{array}{*{20}{l}} A_{,t}=-8 \pi rA^{2}\rm{e}^{-\delta}PQ. \end{array} $
(4) The combination of
$ G^{r}_{r}=8\pi T^{r}_{r} $ and Eq. (3) yields$ \begin{array}{*{20}{l}} \delta_{,r}=-4\pi r(P^{2}+Q^{2}). \end{array} $
(5) With Eq. (2), we obtain
$ \begin{array}{*{20}{l}} Q_{,t}=(A \rm{e}^{-\delta} P)_{,r}. \end{array} $
(6) From the conservation of the energy-momentum tensor,
$ T^{\mu\nu}_{;\mu}=0 $ , we have$ P_{,t}=\frac{1}{r^{2}}(r^{2} A \rm{e}^{-\delta} Q)_{,r}. $
(7) The Misner-Sharp mass is defined as [18]
$ m\equiv\frac{r}{2}(1-g^{\mu\nu}r_{,\mu}r_{,\nu})=\frac{r}{2}(1-A). $
(8) The initial conditions for ϕ are set as
$\phi|_{t_i}= a\exp[-(r/\sigma)^{2}]$ and$ \phi_{,t}|_{t_i}=0 $ . The regularity of Eq. (3) at the center requires that$ A(r=0,t)=1 $ . We choose$\delta(r=0, t)=0$ , which implies that the coordinate time is equal to its proper time at the center. In the simulation, we integrate Eqs. (3) and (5)−(7) using the fourth-order Runge-Kutta method. A mesh refinement algorithm is implemented. We approach the critical solution by fine-tuning the initial profile of the scalar field via the bisection method. For details on the numerics, see Ref. [19]. -
We rewrite the metric (1) as
$ \begin{array}{*{20}{l}} {\rm d} s^{2}=-\alpha^{2}(r,t){\rm d}t^{2}+\beta^{2}(r,t){\rm d}r^{2}+r^{2}{\rm d}\Omega^2. \end{array} $
(9) For convenience, we adjust the time coordinate such that
$ t=0 $ when the naked singularity forms and define$X(r,t)\equiv \sqrt{2\pi}(r/\beta)\phi_{,r}$ ,$ Y(r,t)\equiv\sqrt{2\pi}(r/\alpha)\phi_{,t} $ ,$ \rho\equiv \ln r $ ,$ T\equiv\ln(-t) $ , and$ u\equiv t/r $ . Then, the equations for ϕ (6) and (7) can be respectively rewritten as$ \begin{array}{*{20}{l}} (\beta X)_{,u}=-\alpha Y + (\alpha Y)_{,\rho} -u(\alpha Y)_{,u}, \end{array} $
(10) $ \begin{array}{*{20}{l}} (\beta Y)_{,u}=\alpha X + (\alpha X)_{,\rho}-u(\alpha X)_{,u}. \end{array} $
(11) In critical collapse, the period in terms of the coordinate time t exponentially decreases. Consequently, the metric functions and matter field in the late stage of collapse and large-radius region for which
$ |t/r|\ll 1 $ appear to be "frozen" rather than propagating [20, 21]. In Ref. [17], the authors offered one ansatz: in this region, the last terms in Eqs. (10) and (11) are negligible in comparison with the first terms. Moreover, treating α and β as constant, the authors obtained the following solutions:$ \begin{array}{*{20}{l}} X\approx B\sin[\omega(\rho-\alpha u)-\gamma], \hphantom{dd} Y\approx B\sin[\omega(\rho-\alpha u)], \end{array} $
(12) where
$ 1+\frac{1}{\omega^{2}}=\beta^2, \hphantom{dddd} \sin\gamma=\frac{1}{\omega\beta}, \hphantom{dddd} \cos\gamma=-\frac{1}{\beta}. $
(13) The expressions (12) are consistent with the numerical results. However, some treatments in the above have not been fully justified. In addition, although approximate expressions for X and Y were obtained, the results for the metric functions and scalar field remain absent. We address such issues below.
In Ref. [17], some terms in Eqs. (10) and (11), that is,
$ -u(\alpha Y)_{,u} $ ,$ -u(\alpha X)_{,u} $ ,$ \beta_{,u}X $ ,$ \alpha_{,\rho}Y $ ,$ \beta_{,u}Y $ , and$ \alpha_{,\rho}X $ , were dropped. In fact, as shown in Figs. 1 and 2, in the large-radius region$ (r>10^{-3}) $ , the absolute values of the terms$ -u\alpha_{,u}Y $ ,$ -u\alpha_{,u}X $ ,$ \alpha_{,\rho}Y $ , and$ \alpha_{,\rho}X $ can sometimes be greater than those of other terms. However, the terms dropped approximately cancel. Consequently, the equations constructed by the remaining terms roughly hold:Figure 1. (color online) Numerical results for Eqs. (10) and (14). (a) Results for Eq. (10). (b) Results for Eq. (14). In the large-radius region
$ (r>10^{-3}) $ , the absolute values of$ \alpha_{,\rho}Y $ and$ u\alpha_{,u}Y $ are sometimes greater than those of other terms in Eq. (10). However, the three terms$ \beta_{,u}X $ ,$ -\alpha_{,\rho}Y $ and$ u(\alpha Y)_{,u} $ roughly cancel. Then, Eq. (14) approximately holds.Figure 2. (color online) Numerical results for Eqs. (11) and (15). (a) Results for Eq. (11). (b) Results for Eq. (15).
$ \begin{array}{*{20}{l}} \beta X_{,u}\approx-\alpha Y + \alpha Y_{,\rho}, \end{array} $
(14) $ \begin{array}{*{20}{l}} \beta Y_{,u}\approx\alpha X + \alpha X_{,\rho}. \end{array} $
(15) From this perspective, treating α and β as constant in Ref. [17] is effectively valid.
In the analytic results (12) obtained in Ref. [17], only the phases in the sine functions are functions of r and t, and the amplitudes are constant. We examine the numerical results for ϕ and find that besides the phase, the amplitude for ϕ is also a function of r and t. We find that the field ϕ admits the following approximate expression:
$ \begin{array}{*{20}{l}} \phi(r,t)\approx C_{1}(1+C_{2}[H(r,t)])\cos(\omega\ln r + C_{3}[H(r,t)] + \varphi_{0} ). \end{array} $
(16) The quantity
$ [H(r,t)] $ has the following features:(i) We first define
$ H(r,t) $ in the usual manner:$ H(r,t)\equiv\frac{\omega\alpha t}{r}=\omega A^{1/2} {\rm e}^{-\delta}\frac{t}{r}. $
(17) Then, we have
$ H_{,t}=\frac{\omega\alpha}{r}+\frac{\omega\alpha_{,t}t}{r}+\frac{\omega_{,t}\alpha t}{r}. $
(18) (ii)
$ [H(r,t)] $ is defined as$ [H(r,t)]\equiv\frac{{\bar{\omega}}{\bar{\alpha}} t}{r}. $
(19) Here,
$ \bar{\omega} $ and$ \bar{\alpha} $ are constant values of$ \omega(r,t) $ and$ \alpha(r,t) $ . This is related to the treatment of α and β as constant in the discussions of Eqs. (14) and (15).(iii) From Eq. (16), we obtain the expression for
$ \phi_{,t} $ ,$ \begin{array}{*{20}{l}} \phi_{,t}\approx C_{1}\sqrt{C_{2}^2+C_{3}^2}[H]_{,t}\cos(\omega\ln r +C_{3}[H]+\varphi_{0}+\varphi_{1}), \end{array} $
(20) where
$ \tan\varphi_{1}\equiv C_{3}/C_{2} $ . Regarding the quantity$ H_{,t}(=\omega\alpha/r+ \omega\alpha_{,t}t/r+\omega_{,t}\alpha t/r) $ , the numerical results show that$ |{\omega\alpha_{,t}t}/{r}| $ is sometimes greater than$ {\omega\alpha}/{r} $ . However, comparing expression (20) with the numerical results for$ \phi_{,t} $ , we always obtain$ [H]_{,t}\approx\frac{\omega\alpha}{r}=\omega A^{1/2}{\rm e}^{-\delta}\frac{1}{r}. $
(21) This implies that in
$ [H]_{,t} $ , the contributions from$ \omega\alpha_{,t}t/r $ and$ \omega_{,t}\alpha t/r $ are negligible. This should be related to the fact that the respective reductions of Eqs. (10) and (11) to Eqs. (14) and (15) are equivalent to treating α and$ \beta(\equiv \sqrt{1+\omega^{-2}}) $ as constant.(iv) The numerical results in Fig. 3(a) show that in the large-radius region, the equation of motion for ϕ (7) is reduced to
Figure 3. (color online) Numerical results for the equation of motion for ϕ (7) and the transition region. (a) Results for Eq. (7). In the large-radius region
$ (r>10^{-3}) $ ,$ A^{-1}{\rm e}^{\delta}\phi_{,tt}\approx-(A^{-1}{\rm e}^{\delta})_{,t}\phi_{,t} $ . This is very different from the flat-spacetime form$ \phi_{,tt}=r^{-2}(r^{2}\phi_{,r})_{,r} $ . In the central region$ (r<10^{-5}) $ ,$A^{-1}e^{\delta}\phi_{,tt}\approx A {\rm e}^{-\delta}r^{-2}(r^{2}\phi_{,r})_{,r}$ . Considering that in this region$ A\approx1 $ and$ \delta\approx 0 $ ,$ \phi_{,tt}\approx r^{-2}(r^{2}\phi_{,r})_{,r} $ . (b) Transition region between the central and large-radius regions:$ [r_1,\; r_2] $ . At$ r=r_{1} $ ,$ |C_{3}H|\sim|\omega\ln r| $ . At$ r=r_2 $ ,$ |C_{3}H_{,r}|\sim\omega/r $ .$ \begin{array}{*{20}{l}} A^{-1}{\rm e}^{\delta}\phi_{,tt}\approx-(A^{-1} {\rm e}^{\delta})_{,t}\phi_{,t}. \end{array} $
(22) Using Eq. (22) and the numerical results of
$ |\delta_{,t}|\gg |A_{,t}| $ , we have$ \begin{array}{*{20}{l}} \phi_{,tt}\approx-\delta_{,t}\phi_{,t}. \end{array} $
(23) Combining Eqs. (20), (21), and (23) and the numerical results of
$ |\delta_{,t}|\gg H_{,t} $ generates$ [H]_{,tt}\approx\frac{\omega\alpha_{,t}}{r}\approx -\delta_{,t}[H]_{,t}. $
(24) Namely, we treat α effectively as constant at the first-order accuracy, and the dynamical feature of α begins to take effect since the second-order temporal derivative of
$ [H(r,t)] $ .(v) As shown in Fig. 3(b), at the late stage of critical collapse, in the large-radius region at which
$ |t/r|\ll 1 $ ,$ |H|\ll 1 $ ,$ |H|\ll|\omega\ln r| $ , and$ |H_{,r}|\ll 1/r $ . Therefore, with Eq. (16),$ [H] $ mainly contributes to the temporal derivatives of ϕ, rather than to the field ϕ and its spatial derivatives.The numerical results show that
$ C_{1}\approx0.058 $ ,$ C_{2}^2+C_{3}^2\approx 1 $ , and$ \varphi_{1}\approx 1.08 $ . As shown in Figs. 4(a) and (b), the expressions for ϕ (16),$ \phi_{,t} $ (20), and$ \phi_{,tt} $ (23) agree well with the numerical results. Note that when we compare the analytic expressions with the numerical results in the large-radius region, the tail part, e.g., the region for$ r>1 $ in Fig. 4, is excluded.Figure 4. (color online) Comparison of the analytic and numerical results for the scalar field and metric functions in the large-radius region. (a) Results for ϕ (16) and
$ \phi_{,t} $ (20). (b)$ \phi_{,tt}\approx-\delta_{,t}\phi_{,t} $ . (c) Results for$ m/r $ (27). (d) Results for δ (30).With Eqs. (16) and (20), we can rewrite Eq. (4) as
$ \begin{aligned}[b] \frac{1}{A}\frac{\partial A}{\partial t} =& -8\pi r\phi_{,t}\phi_{,r}\approx C_{4}[H]_{,t}[\sin(2\omega\ln r + 2C_{3}[H] \\ & + 2\varphi_{0} + \varphi_{1}) -\sin\varphi_{1}], \end{aligned} $
(25) where
$ C_4=4\pi\omega{C_{1}^2}\sqrt{C_{2}^2+C_{3}^2} $ . Via integration, we have$ \begin{aligned}[b] \ln A\approx& -\frac{C_4}{2C_3}\cos(2\omega\ln r + 2C_{3}[H] + 2\varphi_{0} + \varphi_{1} )\\ & - C_{4}\sin\varphi_{1}[H] + C_5. \end{aligned} $
(26) Then, using Eq. (8) and the fact that
$ |H|\ll 1 $ , we obtain$ \frac{m}{r}\approx C_{6}\cos(2\omega\ln r+2C_{3}[H]+2\varphi_{0}+\varphi_{1})+C_7, $
(27) where
$C_6\approx {\rm e}^{C_5}C_{4}/(4C_3)\approx {\rm e}^{C_5}\pi\omega{C_{1}^2}\sqrt{C_{2}^2+C_{3}^2}/C_{3}$ and$C_7= (1/2)(1-{\rm e}^{C_{5}})$ . As shown in Fig. 4(c), the expression for$ m/r $ (27) is consistent with the numerical results. The fitting results are$ C_6=0.013360\pm 0.000009\approx 1/75 $ and$ C_7\approx 0.065480\pm 0.000007\approx 1/15 $ .With Eq. (8), we can rewrite Eqs. (3) and (5) as
$ \begin{array}{*{20}{l}} m_{,r}=2\pi r^2 A(P^2+Q^2), \end{array} $
(28) $ r\delta_{,r}=\frac{\partial\delta}{\partial\ln r}=-\frac{2}{1-\dfrac{2m}{r}}m_{,r}. $
(29) Then, the solution for δ can be expressed as
$ \begin{aligned}[b] \delta\approx\;& C_8\ln r +\ln\left(1-\frac{2m}{r}\right)\\ &+C_9\sin(2\omega\ln r+2C_{3}[H]+2\varphi_{0}+\varphi_{1})+\delta_{0}(t), \end{aligned} $
(30) where
$ C_8\approx-{2C_7}/(1-2C_7)-2C_{6}^2 $ and$C_9\approx-(C_6+ 8C_{6}C_{7})/\omega$ . As shown in Fig. 4(d), the expression for δ (30) is consistent with the numerical results.In Ref. [17], the quantities α and β were treated as constant. The approximate expressions for X and Y obtained in this manner agree well with the numerical results. Then, it was stated that in this circumstance, the spacetime is effectively flat. In fact, X and Y are combinations of the metric functions and derivatives of the scalar field, rather than the scalar field. To check whether the spacetime is effectively flat, it may be more appropriate to directly investigate the behavior of the equation of motion for the scalar field (7). As shown in Fig. 3(a), in the large-radius region, Eq. (7) is reduced to Eq. (22), which is clearly different from the flat-spacetime form
$ \phi_{,tt}= r^{-2}(r^{2}\phi_{,r})_{,r} $ . Therefore, the spacetime in this region is not effectively flat. -
As shown in Fig. 3(a), in the central region, the absolute values of the terms
$(A^{-1}{\rm e}^{\delta})_{,t}\phi_{,t}$ and$(A^{-1}{\rm e}^{\delta})_{,r}\phi_{,r}$ in Eq. (7) are considerably lower than those of$A^{-1}{\rm e}^{\delta}\phi_{,tt}$ ,$A{\rm e}^{-\delta}\phi_{,rr}$ , and$(2/r)A{\rm e}^{-\delta}\phi_{,r}$ . Moreover, in this region,$ A\approx1 $ and$ \delta\approx 0 $ . Consequently, Eq. (7) is reduced to the flat-spacetime form$ \phi_{,tt}\approx \frac{1}{r^2}(r^{2}\phi_{,r})_{,r}. $
(31) Regarding Eq. (31), we discuss the following:
(i) Equation (31) implies that in the central region, the scalar field ϕ evolves almost as in flat spacetime, not experiencing gravitational effects.
(ii) Besides critical collapse, we check the evolution of the scalar field in two other types of collapse (dispersion and black hole formation) and obtain similar results as (31).
(iii) The result (31) is closely related to the asymptotic behaviors of the metric functions and scalar field near the center. Under the smoothness requirement at the center, the metric functions and scalar field have the following power series expansions near the center [19]:
$ \begin{array}{*{20}{l}} A\approx 1+A_{2}(t)r^2, \phantom{d}\delta\approx\delta_{2}(t)r^2, \phantom{d}\phi\approx\phi_0(t) + \phi_{2}(t)r^2. \end{array} $
(32) With Eqs. (3), (4), (5), (8), and (32), we obtain the following asymptotic expressions:
$ \begin{aligned}[b]& A_{,t}\approx -16\pi \phi_{,t}\phi_{2}r^2, \hphantom{dddd} \delta_{,t}\approx -4\pi \phi_{,tt}\phi_{,t}r^2,\\ & \phi_{,t}\approx \phi_{0}'(t)+\phi_{2}'(t)r^2, \hphantom{dd}A_{,r}\approx -\frac{8\pi}{3}(\phi_{,t})^2 r,\\ & \delta_{,r}\approx -4\pi(\phi_{,t})^2 r, \hphantom{dddddd} \phi_{,r}\approx 2\phi_{2}(t)r,\\ \end{aligned} $
(33) which are also shown in Fig. 5. With Eqs. (32) and (33), we can straightforwardly simplify Eq. (7) to (31).
Figure 5. (color online) First-order temporal and spacial derivatives for A, δ, and ϕ. As discussed in Eq. (33), near the center,
$ A_{,t}\propto r^2 $ ,$ \delta_{,t}\propto r^2 $ ,$ \phi_{,t}\approx \phi_{0}'(t)+\phi_{2}'(t)r^2 $ ,$ A_{,r}\propto r $ ,$ \delta_{,r}\propto r $ , and$ \phi_{,r}\propto r $ .(iv) It is known that in critical collapse, the Ricci curvature scalar R in the central region is very high and will eventually diverge. This does not contradict the result in (31) because Eq. (31) is caused by the fact that the first-order derivatives of the metric components asymptote to zero. Conversely, as discussed below, the major terms constructing R include the second-order derivatives of the metric components, first-order derivatives of the metric components divided by r, and
$ 2(1-A) $ divided by$ r^2 $ , which are very large and will eventually diverge.For the metric (1), the Ricci curvature scalar can be written as
$ \begin{aligned}[b] R=\;&\frac{4A\delta_{,r}}{r} - \frac{4A_{,r}}{r} + 2A\delta_{,rr} + \frac{2(1-A)}{r^2} - A_{,rr} - \frac{A_{,tt} {\rm e}^{2\delta}}{A^2}\\ &+ 3A_{,r}\delta_{,r} - 2A(\delta_{,r})^2 + \frac{2(A_{,t})^2 {\rm e}^{2\delta}}{A^3} - \frac{A_{,t}\delta_{,t}{\rm e}^{2\delta}}{A^2}. \end{aligned} $
(34) With Eqs. (3), (4), (5), (8), (32), and (33), we obtain asymptotic expressions for all the terms on the right-hand side of Eq. (34):
$ \begin{aligned}[b] &\frac{4A\delta_{,r}}{r}\approx -2D,\hphantom{dd}- \frac{4A_{,r}}{r}\approx\frac{4}{3}D,\hphantom{dd}2A\delta_{,rr}\approx -D,\\ &\frac{2(1-A)}{r^2}\approx- A_{,rr}\approx \frac{D}{3}, \hphantom{dd}\rm{where}\hphantom{d} D=8\pi(\phi_{,t})^2. \\& -\frac{A_{,tt}{\rm e}^{2\delta}}{A^2}\approx 16\pi \phi_{,tt}\phi_{2}r^2,\\ &3A_{,r}\delta_{,r}\approx 32\pi^2 (\phi_{,t})^4 r^2,\\& -2A(\delta_{,r})^2\approx -32\pi^2 (\phi_{,t})^4 r^2,\\& \frac{2(A_{,t})^2 {\rm e}^{2\delta}}{A^3}\approx 512\pi^2 (\phi_{,t})^2 (\phi_{2})^2 r^4, \end{aligned} $
$ \begin{aligned}[b] -\frac{A_{,t}\delta_{,t} {\rm e}^{2\delta}}{A^2}\approx -64\pi^2 \phi_{,tt}(\phi_{,t})^2 \phi_{2} r^4. \end{aligned} $
The first five terms are dominant and have the same order of magnitude as
$ 8\pi(\phi_{,t})^2 $ , and the remaining terms are proportional to$ r^2 $ or$ r^4 $ and are negligible.As shown in Fig. 3(b), the transition region between the central and large-radius regions can be expressed as
$ r\in [r_1,\; r_2] $ . At$ r=r_{1} $ ,$ |C_{3}H|\sim|\omega\ln r| $ ; at$ r=r_2 $ ,$ |C_{3}H_{,r}|\sim \omega/r $ .
New results on the dynamics of critical collapse
- Received Date: 2024-01-27
- Available Online: 2024-06-15
Abstract: We study the dynamics of the critical collapse of a spherically symmetric scalar field. Approximate analytic expressions for the metric functions and matter field in the large-radius region are obtained. In the central region, owing to the boundary conditions, the equation of motion for the scalar field is reduced to the flat-spacetime form.