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Various modified gravity theories have been proposed to extend general relativity. The
$ f(R,T) $ gravity model [46], which originates from the combination of curvature-matter coupling theory, has many applications in describing the current Universe. Let us start from the$ f(R,T) $ action given by$ {\cal{A}} = \frac{1}{16\pi}\int f(R,T)\sqrt{-g}\mathrm{d}^4x + \int{\cal{L}}_m \sqrt{-g}\mathrm{d}^4x , $
(1) where g is the determinant of the metric
$ g_{\mu\nu} $ , and$ {\cal{L}}_m $ denotes the action of matter.$ f(R,T) $ is an arbitrary function of the Ricci scalar R (Ricci scalar) and T (trace of the energy-momentum tensor).Variations in action (1) with respect to metric
$ g_{\mu\nu} $ lead to the modified field equations of$ f(R,T) $ gravity, yielding$\begin{aligned}[b]& f_R(R,T) R_{\mu\nu} - \dfrac{1}{2}f(R,T) g_{\mu\nu} + [g_{\mu\nu}\square - \nabla_\mu\nabla_\nu] f_R(R,T)\\ =\; &8\pi T_{\mu\nu} -(T_{\mu\nu} + \Theta_{\mu\nu})f_T(R,T) , \end{aligned}$
(2) where
$ f_R \equiv \partial f/\partial R $ ,$ f_T \equiv \partial f/\partial T $ , and$ \square \equiv \nabla_\mu\nabla^\mu $ is the d'Alembertian operator with a covariant derivative represented by$ \nabla_\mu $ . Here, the auxiliary tensor$ \Theta_{\mu\nu} $ is defined in terms of the variation in$ T_{\mu\nu} $ as$ \Theta_{\mu\nu} \equiv g^{\alpha\beta}\frac{\delta T_{\alpha\beta}}{\delta g^{\mu\nu}} = -2T_{\mu\nu} + g_{\mu\nu}{\cal{L}}_m - 2g^{\alpha\beta} \frac{\partial^2{\cal{L}}_m}{\partial g^{\mu\nu} \partial g^{\alpha\beta}} . $
(3) Taking the trace of the field equations (2), we can obtain a relation between R and T of the form
$ 3\square f_R(R,T) + Rf_R(R,T) - 2f(R,T) = 8\pi T - (T+\Theta)f_T(R,T) , $
(4) where
$ \Theta = g^{\mu\nu}\Theta_{\mu\nu} $ is the trace of$ \Theta_{\mu\nu} $ . Finally, we obtain the covariant derivative of the stress-energy tensor and use the field equations in (2), which yield [90]$\begin{aligned}[b] \nabla^\mu T_{\mu\nu} = \;& \ \frac{f_T(R,T)}{8\pi - f_T(R,T)}\\ & \times\bigg[ (T_{\mu\nu} + \Theta_{\mu\nu})\nabla^\mu \ln f_T(R,T) + \nabla^\mu\Theta_{\mu\nu} - \frac{1}{2}g_{\mu\nu}\nabla^\mu T \bigg] . \end{aligned}$
(5) Interestingly, Eq. (5) is not conserved owing to the interaction between the curvature and matter sectors. Moreover, non-conservation leads to nongeodesic motion of particles. In the case of
$ f(R,T) $ gravity, the functional form of f is not unique. Many$ f(R,T) $ models exhibit interesting features; however, we continue our investigation by considering the simplest functional form of$ f(R,T) = R+ 2\beta T $ [46], i.e., the usual Einstein-Hilbert term plus a T dependent function$ f(T ) $ . This model has been widely applied in astrophysical scenarios and also explains the accelerated expansion of the Universe in an elegant manner. Using the particular form function, we rewrite Eqs. (2), (4), and (5) as$ G_{\mu\nu} = 8\pi T_{\mu\nu} + \beta Tg_{\mu\nu} - 2\beta(T_{\mu\nu} + \Theta_{\mu\nu}) , $
(6) $ R = -8\pi T - 2\beta(T- \Theta) , $
(7) $ \nabla^\mu T_{\mu\nu} = \frac{2\beta}{8\pi - 2\beta} \left[ \nabla^\mu \Theta_{\mu\nu} - \frac{1}{2}g_{\mu\nu}\nabla^\mu T \right] , $
(8) where
$ G_{\mu\nu} $ is the Einstein tensor. -
To study the WH structure, we start by considering the static spherically symmetric metric ansatz in Schwarzschild coordinates in the form
$ \mathrm{d}s^2 = -e^{2\Phi(r)}\mathrm{d}t^2+\frac{\mathrm{d}r^2}{1-\dfrac{b(r)}{r}}+r^2(\mathrm{d}\theta^2+\sin^2\theta \mathrm{d}\phi^2), $
(9) which is in the form of the MT metric [2]. Here,
$ \Phi(r) $ is known as the redshift function, and$ b(r) $ is the shape function. The range of the radial coordinate r is$ r\geqslant {r_0} $ , with a minimum value at$ b(r_0) = r_0 $ . This can be interpreted as the ‘throat’ of the WH, with the circumference of a circle given by$ 2\pi r $ . More precisely, the shape function should satisfy the flaring-out condition, i.e.,$ \dfrac{b(r)-rb^{\prime}(r)}{b^2(r)}>0 $ [2], which is provided by the mathematics of embedding. This implies another restriction$ b^{\prime}(r_0) < 1 $ at the throat. In addition, the shape function obeys$ b(r)-r \leqslant 0 $ . Nevertheless,$ \Phi(r) $ must be finite everywhere to ensure the absence of an event horizon.Here, we adopt an anisotropic fluid form that describes the matter sector. Such a tensor can be written as
$ T_{\mu\nu} = (\rho+p_t)u_\mu u_\nu+ p_t g_{\mu\nu}-\sigma \chi_{\mu}\chi_{\nu}, $
(10) where
$ \rho = \rho(r) $ is the energy density,$ p_r = p_r(r) $ and$ p_t = p_t (r) $ are the radial and transverse pressures, respectively,$ u^\mu $ is the 4-velocity,$ \chi^{\mu} $ is the unit radial vector with$ \chi_{\mu}\chi^{\mu} = 1 $ , and$ g_{\mu\nu} $ is the metric tensor. The anisotropy factor is given by$ \sigma = p_t-p_r $ .It is well known from the definition of the matter Lagrangian for isotropic/anisotropic fluid that the energy-momentum tensor is not unique. We can choose either
$ {\cal{L}}_m = {\cal{P}} $ or$ {\cal{L}}_m = -\rho $ . In this study, we consider$ {\cal{L}}_m = {\cal{P}} $ , where$ {\cal{P}} \equiv (p_r+ 2p_t)/3 $ [91−93], which allows us to rewrite Eq. (3) as$ \Theta_{\mu\nu} = -2T_{\mu\nu} + {\cal{P}}g_{\mu\nu} $ . By taking the covariant divergence of Eq. (8), we obtain the result$ \nabla^\mu T_{\mu\nu} = \frac{2\beta}{8\pi + 2\beta} \left[ \nabla^\mu \left({\cal{P}}g_{\mu\nu} \right) - \frac{1}{2} \nabla_\nu T \right] . $
(11) Note that the standard conservation equation does not hold for this theory. If we take
$ \beta = 0 $ , we can recover the conservation of the energy-momentum tensor for the general relativistic case. Finally, combining Eqs. (9) and (10) and the gravitational equation (6), we obtain the following expressions:$ 8\pi\rho + \beta\left[ 3\rho - p_r - \frac{2}{3}\sigma \right] = \frac{b^{\prime}}{r^{2}} , $
(12) $ 8\pi p_r + \beta\left[ -\rho + 3p_r+ \frac{2}{3}\sigma \right] = 2\left(1-\frac{b}{r}\right)\frac{\Phi^{\prime}}{r}-\frac{b}{r^{3}} , $
(13) $ \begin{aligned}[b]& 8\pi p_t + \beta\left[ -\rho + 3p_r+ \frac{8}{3}\sigma \right]\\ =\;& \left(1-\frac{b}{r}\right)\left[\Phi^{\prime\prime}+\Phi^{\prime 2}-\frac{b^{\prime}r-b}{2r(r-b)}\Phi^{\prime}-\frac{b^{\prime}r-b}{2r^2(r-b)} +\frac{\Phi^{\prime}}{r}\right] , \end{aligned}$
(14) where the prime stands for differentiation with respect to r. Finally, we have three independent Eqs. (12)–(14) with five unknown quantities, i.e.,
$ \Phi(r) $ ,$ b(r) $ ,$ \rho(r) $ ,$ p_r(r) $ , and$ p_t(r) $ . Evidently, this system is underdetermined, and we are free to make any two assumptions to generate a physically reasonable WH solution.For the sake of simplicity, we can consider an EoS of the form [12]
$ \rho(r) = \omega \left[p_r+2p_t\right]. $
(15) With these considerations, we may express the EM tensor using Eq. (15) as
$ T = -\rho+p_r+ 2p_t = \rho(1-\omega)/ \omega $ . In particular, the EoS (15) reduces to a traceless EoS, i.e.,$ T = 0 $ for$ \omega = 1 $ , and the situation is related to the Casimir effect. By choosing this particular EoS, the authors of [94, 95] have reported WH solutions in higher dimensional gravity theory. Most importantly, this EoS has the feature of necessarily violating the NEC, which is required to maintain the throat of a WH in the open position via the repulsive gravitational effect induced by the negative density. In light of these considerations, i.e.,$ \omega = 1 $ , we endeavor to construct WH models in the context of$ f(R,T) $ gravity. -
This section is devoted to discussing some properties of the stress-energy tensor that will be useful when analyzing the energy conditions. The violation of the NEC, at least in a neighborhood, is the most salient feature of these space-times from the perspective of general relativity [2]. As a result, we search for the existence of WH solutions in
$ f(R,T) $ theory with suitable energy conditions such that the matter field violates the NEC. Given the stress-energy tensor (10), the NEC is given by$ \rho+p_i \geqslant 0,~~ \text{where}~~ i = r, t, $
(16) whereas the WEC asserts that
$ \rho \geqslant 0 ~~ \text{and} ~~ \rho+p_i \geqslant 0, $
(17) and the expression for the SEC implies
$ \rho +\sum\limits_{i} p_i \geqslant 0 ~~ \text{and for each} ~~ \rho+p_i\geqslant 0. $
(18) The above expressions prove useful when searching for WH solutions with NEC violation preferably not originating from exotic matter, such as dark energy.
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Here, we begin by finding WH solutions with two different types of redshift functions and one shape function, considering that
$ f(R,T) = R+ 2\beta T $ . For the WH to be traversable, we consider$ \Phi^{\prime}(r) = 0 $ and$ \Phi(r) = \log \left(1+\dfrac{r_0}{r}\right) $ . This choice guarantees that the redshift function is finite everywhere, and consequently, the geometry is horizon free. Finally, we consider the shape function$ b(r) = \dfrac{r_0^2}{r} $ , which ensures an asymptotically flat spacetime satisfying the flaring-out condition at the WH throat. These assumptions simplify the field equations significantly and provide particularly intriguing solutions, as shown below. -
The simplest approach is to consider
$ \Phi^{\prime}(r) = 0 $ , implying WHs with zero tidal forces. In this context, Eqs. (12)–(14) with EoS (15) provide the system$ \frac{b'(r)}{r^2} = \frac{8}{3} \left[\beta +3 \pi ) (p_r+2 p_t\right], $
(19) $ -\frac{b(r)}{r^3} = \frac{4}{3} \left[(\beta +6 \pi ) p_r-\beta p_t\right], $
(20) $ \frac{b-r b'}{2 r^3} = \frac{2}{3} \left[(\beta +12 \pi ) p_t-\beta p_r\right]. $
(21) From the system of Eqs. (19)–(21), we may express
$ p_r $ and$ p_t $ in terms of b and$ b^{\prime} $ in the form$ p_r(r) = \frac{\beta r b'-4 (\beta +3 \pi ) b}{8 (\beta +3 \pi ) (\beta +4 \pi ) r^3}, $
(22) $ p_t(r) = \frac{(\beta +6 \pi ) r b'+2 (\beta +3 \pi ) b}{8 (\beta +3 \pi ) (\beta +4 \pi ) r^3}. $
(23) Substituting
$ p_r $ and$ p_t $ given in Eqs. (21)–(23), we obtain the shape function$ b(r) = C $ . Using the condition$ b(r_0 ) = r_0 $ , we can write$ b(r) = r_0 $ , which is constant. Substituting these values into Eqs. (19)–(20), we obtain the components of the energy-momentum tensor$ \rho(r) = 0 $ ,$ p_r(r) = -\dfrac{r_0}{2 (\beta +4 \pi ) r^3} $ , and$ p_t(r) = \dfrac{r_0}{4 (\beta +4 \pi ) r^3} $ . This is a physically untenable situation because the energy density is zero while$ p_r = -2p_t $ . Thus, considering$ \Phi^{\prime}(r) = 0 $ is not suitable for describing spherically symmetric WH solutions in$ f(R,T) $ gravity. Interestingly, zero-tidal-force WHs with isotropic pressure and a single matter source are also not possible in general relativity (see Ref. [7]). -
The second case we consider is logarithmic:
$\Phi(r) = \log \left(1+\dfrac{r_0}{r}\right)$ . In this model, the field equations (12)–(14) with EoS (15) reduce to the system$ \frac{b'}{r^2} = \frac{8}{3} \left[\beta +3 \pi \right] \left[p_r+2 p_t\right], $
(24) $ \frac{b (r_0-r)-2 r r_0}{r^3 (r+r_0)} = \frac{4}{3} \left[(\beta +6 \pi ) p_r-\beta p_t\right], $
(25) $ \frac{r \left[2 r_0-r b'\right]+b (r-2 r_0)}{2 r^3 (r+r_0)} = \frac{2}{3} \left[(\beta +12 \pi ) p_t-\beta p_r\right]. $
(26) Now, the first two equations give the expressions for
$ p_r $ and$ p_t $ in terms of b and$ b^{\prime} $ ,$ p_r(r) = \frac{\beta r (r+r_0) b'-4 (\beta +3 \pi ) (b (r-r_0)+2 r r_0)}{8 (\beta +3 \pi ) (\beta +4 \pi ) r^3 (r+r_0)}, $
(27) $ p_t(r) = \frac{(\beta +6 \pi ) r (r+r_0) b'+2 (\beta +3 \pi ) (b (r-r_0)+2 r r_0)}{8 (\beta +3 \pi ) (\beta +4 \pi ) r^3 (r+r_0)}. $
(28) Substituting the expressions for
$ p_r $ and$ p_t $ into Eq. (27), we arrive at the following master equation:$ b'(r) = -\frac{(\beta +3 \pi ) r_0 b}{r [\beta r+3 \pi (2 r+r_0)]}. $
(29) Eq. (29) is routinely solved in the form
$ b(r) = r_0 \left[\frac{ 6\pi r+3 \pi r_0+ \beta r}{(\beta +9\pi)r }\right]^{{(3\pi+\beta)}/{(3\pi)}}, $
(30) using the condition
$ b(r_0) = r_0 $ . At the throat,$b'(r_0) = \dfrac{6 \pi }{\beta +9 \pi }-1 < 1$ . This imposes the restriction$ -6 \pi <\beta <-3 \pi $ , for which$ 0< b'(r_0)<1 $ . Moreover, we verify that$ \dfrac{b(r)}{r}\to 0 $ as$ r\to \infty $ , which confirms the asymptotic flatness. Using Eq. (30), we plot the shape function for$ \beta = -4.5 \pi $ (dot-dashed),$ \beta = -5\pi $ (dashed), and$ \beta = -5.5 \pi $ (dotted) in the left panel of Fig. 1, when$ r_0 = 1 $ .Figure 1. (color online) Left panel: Behavior of
$ b(r) = r $ (solid black), and other curves are plotted for$ b(r) $ given in Eq. (30), which shows$ b(r) < r $ . Here, we consider a specific redshift function$ \Phi(r) = \log \left(1+\dfrac{r_0}{r}\right) $ and plot$ b(r) $ for$ \beta = -4.5 \pi $ (solid),$ \beta = - 5\pi $ (dashed), and$ \beta = -5.5 \pi $ (dot-dashed). Middle panel: Using Eqs. (30) and (31), we plot the embedded diagram, which provides valuable insights into the geometry and topology of the WH configurations. Right panel: Using Eqs. (30) and (31), we plot the embedded surface$ z(r) $ , which provides valuable insights into the geometric structure and characteristics of the embedded surface. In all cases, we consider$ \omega = 1 $ , which reduces to a traceless EMT, with$ T = 0 $ . See the text for specific choices of the considered parameters.To better understand the shape function, we find the equation for the embedding surface,
$ \frac{\mathrm{d}z}{\mathrm{d}r} = \pm \left(\frac{r}{b(r)}-1\right)^{-1/2}. $
(31) In Fig. 1 (middle and right panels), we present the embedding diagram and embedded surface
$ z(r) $ with Eqs. (30) and (31). The location of the WH throat is defined by the black ring that connects two distinct universes.Using Eqs. (27)–(28) and Eq. (30), we find the following relationships:
$ \rho = -\frac{3 r_0^2}{8 (\beta +9 \pi ) r^4}u(r) , $
(32) $ \rho+ p_r = -\frac{r_0 \left(\beta \left(r^2+r_0^2\right)+6 \pi r^2\right) u(r)+2 (\beta +9 \pi ) r^2 r_0}{2 (\beta +4 \pi ) (\beta +9 \pi ) r^4 (r+r_0)}, $
(33) $ \rho + p_t = \frac{r_0 \left((\beta+6 \pi) \left(r^2- 3 r r_0- 2 r_0^2\right) \right) u(r) + 2 (\beta +9 \pi ) r^2 r_0}{4 (\beta +4 \pi ) (\beta +9 \pi ) r^4 (r+r_0)}, $
(34) where
$u(r) = \left(\dfrac{\beta r+6 \pi r+3 \pi r_0}{\beta r+9 \pi r}\right)^{{\beta }/{(3 \pi )}}$ . For$ r> r_0 = 1 $ , we plot ρ,$ \rho+p_r $ , and$ \rho+p_t $ as functions of r in Fig. 2. It is clear that both$ \rho+p_r $ and$ \rho+p_t $ tend to zero as$ r \to \infty $ . For$ -6 \pi <\beta <-3 \pi $ , energy density is negative outside the throat while$ \rho+p_r >0 $ and$ \rho+p_t <0 $ . As shown in Fig. 2 , the NEC is violated outside the throat. The parameters of the solution are$ -6 \pi <\beta <-3 \pi $ and$ r_0 = 1 $ .Figure 2. (color online) Here, we consider a specific redshift function
$ \Phi(r) = \log \left(1+\dfrac{r_0}{r}\right) $ and plots of the specific stress-energy profile for ρ (Left panel),$ \rho+p_r $ (Middle panel), and$ \rho+p_t $ (Right panel) versus r. In all cases, we consider$ \omega = 1 $ , which reduces to a traceless EMT, with$ T = 0 $ . See the text for specific choices of the considered parameters.At the throat,
$ r = r_0 $ , we have$ (\rho+ p_r)|_{r_0} = -\frac{\beta +6 \pi }{(\beta +4 \pi ) (\beta +9 \pi ) r_0^2}, $
(35) $ (\rho+p_t)|_{r_0} = -\frac{\beta }{4 (\beta +4 \pi ) (\beta +9 \pi ) r_0^2} $
(36) It is evident that
$ (\rho+ p_r)|_{r_0} \gtrless 0 $ depending on the values of$ -6 \pi <\beta < -3 \pi $ . In the region$ -4 \pi <\beta < -3 \pi $ , we have$ (\rho+ p_r)|_{r_0} < 0 $ , and$ (\rho+ p_r)|_{r_0} > 0 $ for$ -6 \pi <\beta < -4 \pi $ . Moreover, the situation is merely reversed for the NEC along the transverse direction (at the throat), i.e.,$ (\rho+ p_t)|_{r_0} \lessgtr 0 $ . Note that equations are not-valid for$ \beta = -4 \pi $ . From these observations, we can infer that the model violates the NEC throughout the spacetime, and consequently, WEC violation also occurs.Here, we are also interested in quantifying the total amount of exotic matter through the ''volume integral quantifier'' (VIQ) used by Kar and Sahdev [96]. This can be achieved through the definite integral (with a cut-off of the stress-energy at
$ a>r_0 $ ):$ I_V = \int\left(\rho+p_r\right)\mathrm{d}V = 2\int^{a}_{r_0}\left(\rho+p_r\right)4\pi r^2 \mathrm{d}r, $
(37) and using Eq. (33), we have
$ I_V = \left. \frac{4 \pi r_0 u(r) v(r) \left(3 \pi n(r) r l(r)-6 \pi (\beta +3 \pi )^2 r (v(r))^{-1} m(r)+\beta ^2 p(r) (v(r))^{-1}\right)}{\beta (\beta +3 \pi ) (\beta +4 \pi ) (\beta +9 \pi ) r} -\frac{8 \pi r_0 \log (r+r_0)}{(\beta +4 \pi ) } \right|_{r_0}^{a}, $ (38) where
$ v(r) = \left(\frac{(\beta +6 \pi ) r}{3 \pi r_0}+1\right)^{-\frac{\beta }{3 \pi }}, $
(39) $ l(r) = \, _2F_1\left(-\frac{\beta }{3 \pi },-\frac{\beta }{3 \pi };1-\frac{\beta }{3 \pi };-\frac{r (\beta +6 \pi )}{3 \pi r_0}\right), $
(40) $ m(r) = \, _2F_1\left(-\frac{\beta }{3 \pi },-\frac{\beta }{3 \pi };1-\frac{\beta }{3 \pi };-\frac{r (\beta +6 \pi )}{3 \pi r_0}\right), $
(41) $ n(r) = \beta ^2+9 \pi \beta +18 \pi ^2, $
(42) $ p(r) = \beta r+3 \pi (2 r+r_0). $
(43) After carefully reviewing Eq. (38), we can conclude that
$I_V = \int\left(\rho+p_r\right)\mathrm{d}V \to 0$ when taking the limit$ a \to r_0 $ . For more clarity, we plot Fig. 3, which shows that we can theoretically construct a traversable WH with a small amount of NEC violating matter within the specified range$ -6 \pi <\beta <-3 \pi $ . -
Here, we consider a widely used specific form function given by
$ b(r) = \dfrac{r_0^2}{r} $ . Notably a generalized version of this shape function appears in the work of Tripathy [97]. However, in his study, the author commenced by referring to 'tideless' forces amounting to$ \phi = 0 $ . Thereafter, he adopted the classical Casimir force variation density as$ -\dfrac{1}{a^4} $ , where a is the separation between two charged plates. Based on these, he obtained the shape function above. In addition, he was interested in quantum effects and the generalized uncertainty principle (GUP). Zubair et al. [98] followed a similar approach to Tripathy; however, to fix the geometry of the models, they assumed the existence of conformal Killing vectors. This placed a restriction on the metric potentials, that is, on the shape function profile. Our approach is different. We take the conventional understanding of vanishing tidal forces as$\dfrac{\mathrm{d}\phi}{\mathrm{d}r} = 0$ and then postulate forms of the shape function with the desired properties for a viable WH. In Fig. 4, we plot the shape function$ b(r) $ along with the embedding diagram and embedded surface$ z(r) $ using$ b(r) = \dfrac{r_0^2}{r} $ and Eq. (31).Figure 4. (color online) Left panel: Behavior of
$ b(r) = r $ (solid black), and other curves are plotted for$ b(r) $ given by$b(r) = {r_0^2}/{r}$ , which shows$ b(r) < r $ . Middle panel: Using the shape function$b(r) = {r_0^2}/{r}$ and Eq. (31), we plot the embedded diagram, which provides valuable insights into the geometry and topology of the WH configurations. Right panel: Using the shape function$b(r) = {r_0^2}/{r}$ and Eq. (31), we plot the embedded surface$ z(r) $ , which provides valuable insights into the geometric structure and characteristics of the embedded surface. In all cases, we consider$ \omega = 1 $ , which reduces to a traceless EMT, with$ T = 0 $ . See the text for specific choices of the considered parameters.Considering Eqs. (12)–(14) with EoS (15), we obtain the following expressions:
$ -\frac{r_0^2}{r^4} = \frac{8}{3} [\beta +3 \pi ] [p_r+2 p_t], $
(44) $ \frac{2 \left(r^3-r r_0^2\right) \Phi '-r_0^2}{r^4} = \frac{4}{3} [(\beta +6 \pi ) p_r-\beta p_t], $
(45) $\frac{\left(r^4 - r^2 r_0^2\right) \left(\Phi '' + (\Phi ')^2\right) + r^3 \Phi ' + r_0^2}{r^4} = \frac{2}{3} [(\beta + 12 \pi ) p_t - \beta p_r]. $
(46) Solving Eqs. (44)–(72), we obtain the expressions for
$ p_r $ and$ p_t $ in terms of b and$ b^{\prime} $ ,$ p_r(r) = \frac{8 (\beta + 3 \pi ) r (r - r_0) (r + r_0) \Phi ' - (5 \beta + 12 \pi ) r_0^2}{8 (\beta +3 \pi ) (\beta +4 \pi ) r^4}, $
(47) $ p_t(r) = \frac{4 (\beta +3 \pi ) r (r_0-r) (r+r_0) \Phi '+\beta r_0^2}{8 (\beta +3 \pi ) (\beta +4 \pi ) r^4}, $
(48) and substituting
$ p_r $ and$ p_t $ into Eq. (73), we obtain the following relationship:$\begin{aligned}[b]& 2 \Phi ' \left(2 r^2+r (r-r_0) (r+r_0) \Phi '-r_0^2\right) +\frac{(\beta +6 \pi ) r_0^2}{(\beta +3 \pi ) r}\\ &\quad+2 r (r-r_0) (r+r_0) \Phi ''(r) = 0, \end{aligned}$
(49) which may be integrated to yield the solution
$ \Phi(r) = \ln \left\{\cos \left[\frac{{\cal{A}}}{{\sqrt{2} r_0}} \cot ^{-1}\left(\frac{r_0}{\sqrt{r^2-r_0^2}}\right)-c_1\right]\right\}+c_2 ,\\ $
(50) where
$ {\cal{A}} = \sqrt{\dfrac{(\beta +6 \pi ) r_0^2}{\beta +3 \pi }} $ , and$ c_1 $ and$ c_2 $ are integration constants, which, at the throat, reduce to$ \Phi(r_0) = \ln \left(\cos \left(c_1\right)\right)+c_2. $
(51) We must impose the condition
$ \cos\left(c_1\right) >0 $ to ensure a regular solution. Thus,$ \Phi(r) $ is finite at the throat. Moreover, we know that the range of$ \cos(x) $ is$ -1\leqslant \cos(x) \leqslant 1 $ , and$ \ln(x) $ exists only when$ x >0 $ . Then, the proposed range of$0 < \cos (x) = \cos \left[ {{\cal{A}}}/{{(\sqrt{2} r_0)}} \cot ^{-1}\left( {r_0}/{\sqrt{r^2-r_0^2}} \right)-c_1 \right] \leqslant 1$ , for which$ \ln(x) $ is defined. If we consider the maximum value of$ \cos \left(x\right) = 1 $ , then$ \ln(x) = 0 $ . Moreover,$\cot ^{-1}\left({r_0}/{\sqrt{r^2-r_0^2}}\right) \to \cot ^{-1}(0) = {\pi}/{2}$ as$ r\to \infty $ . This gives$\ln\left[ \cos \left(\dfrac{\pi}{2} \dfrac{{\cal{A}}}{{\sqrt{2} r_0}} -c_1\right)\right]$ a finite value, as the range of$ \cos (x) $ is finite. Finally, we arrive at the conclusion that$ \Phi(r) $ given in Eq. (78) is finite as$ r\to \infty $ ; therefore, this solution now reflects a traversable WH.Considering the redshift function (78) and inserting the field equations (74)–(75) into Eq. (15), we obtain
$ \rho = -\frac{3 r_0^2}{8 (\beta +3 \pi ) r^4}, $
(52) $ \rho+ p_r = \frac{\sqrt{2} \sqrt{(r^2-r_0^2)} {\cal{A}} \tan\theta -2 r_0^2}{2 (\beta +4 \pi ) r^4}, $
(53) $ \rho+p_t = -\frac{\sqrt{2} \sqrt{(r^2-r_0^2)} {\cal{A}} \tan \theta +{\cal{A}}^2}{4 (\beta +4 \pi ) r^4}, $
(54) where
$ {\cal{A}} = \sqrt{\dfrac{(\beta +6 \pi ) r_0^2}{\beta +3 \pi }} $ , and$\theta = \dfrac{1}{\sqrt{2} r_0}\bigg[\sqrt{2} r_0 c_1-{\cal{A}} \cot ^{-1} $ $ \bigg(\dfrac{r_0}{\sqrt{r^2-r_0^2}}\bigg)\bigg] $ . In Fig. 5, we plot ρ,$ \rho+p_r $ , and$ \rho+p_t $ . For this case, we plot a diagram considering different values of β. From Fig. 4, we see that the energy density and two components for$ \rho+p_r $ and$ \rho+p_t $ are negative outside the throat, i.e.,$ r> r_0 = 1 $ . This means that the NEC is always violated outside the throat radius for$ \beta > -3 \pi $ . For the configurations with$ \beta < -6 \pi $ , it is interesting that the WEC (and also the NEC) is satisfied, as shown in the right panel of Fig. 4. Note that$ -6 \pi<\beta < -3 \pi $ is not an allowable range for WH construction from the form of$ {\cal{A}} $ .Figure 5. (color online) Here, we consider a specific shape function
$ b(r) = \dfrac{r_0^2}{r} $ and plots of the specific stress-energy profile for ρ (Left panel),$ \rho+p_r $ (Middle panel), and$ \rho+p_t $ (Right panel) versus r. In all cases, we consider$ \omega = 1 $ , which reduces to a traceless EMT, with$ T = 0 $ . See the text for specific choices of the considered parameters.The NEC at the throat is given by
$ (\rho+ p_r)|_{r_0} = -\frac{1}{(\beta +4 \pi ) r_0^2}, $
(55) $ (\rho+ p_t)|_{r_0} = -\frac{\beta +6 \pi }{4 (\beta +3 \pi ) (\beta +4 \pi ) r_0^2}. $
(56) It is clear that
$ (\rho+ p_{r,t})|_{r_0} <0 $ when$ \beta > -3 \pi $ . Thus, the NEC is always violated for$ \beta > -3 \pi $ . Conversely, we can verify that$ (\rho+ p_{r,t})|_{r_0} >0 $ for$ \beta < -6 \pi $ . This would imply that ρ,$ \rho+p_r $ , and$ \rho+p_t $ are always positive when$ \beta < -6 \pi $ . As a closing remark, we state that realistic physical mechanisms such as the Casimir effect exist to support the geometry of traversable WHs. Therefore, exotic matter fields in the form of dark energy are not necessary. This is important because experimental support for dark energy is absent to date, whereas the Casimir phenomenon is a laboratory proven counter-intuitive effect.We now consider the VIQ to evaluate the total amount of exotic matter. Using Eqs. (53) and (37), we can discuss the amount of exotic matter. The full analytical integration is not feasible because of the complicated nature of the expressions. Thus, we perform numerical integration for specific values of
$ \beta = -2 \pi $ and$ c_1 = 1 $ with$ \tan \theta \approx \theta $ for small values of θ. Finally, we have$ I_V = 2\int^{a}_{r_0}\left(\rho+p_r\right)4\pi r^2 \mathrm{d}r \approx \frac{\sqrt{2} \left(a^2-r_0^2\right)^{3/2} {\cal{A}}}{6 (\beta +4 \pi ) a^3 r_0^2}. $
(57) As a result,
$ I_V \to 0 $ when$ a\to r_0 $ . For greater transparency, we plot Fig. 6 for the range$ -3\pi<\beta<0 $ , where we find that$ \rho+p_r<0 $ . -
Here, we consider the specific model for
$ b(r) = r_0+\gamma r_0 \left(1-\dfrac{r_0}{r}\right) $ [99], where$ 0 < \gamma< 1 $ is of particular interest in generating WH solutions satisfying the condition$ b'(r_0)<1 $ . In Fig. 7, we plot the shape function$ b(r) $ along with the embedding diagram and embedded surface$ z(r) $ corresponding to the above-mentioned shape function. Now, we take the field equations (12)–(14) with EoS (15) to obtainFigure 7. (color online) Left panel: Behavior of
$ b(r) = r $ (solid black), and other curves are plotted for$ b(r) $ given by$ b(r) = \dfrac{r_0^2}{r} $ , which shows$ b(r) < r $ . Middle panel: Using the shape function$ b(r) = r_0+\gamma r_0 \left(1-\dfrac{r_0}{r}\right) $ and Eq. (31), we plot the embedded diagram, which provides valuable insights into the geometry and topology of the WH configurations. Right panel: Using the shape function$ b(r) = r_0+\gamma r_0 \left(1-\dfrac{r_0}{r}\right) $ and Eq. (31), we plot the embedded surface$ z(r) $ , which provides valuable insights into the geometric structure and characteristics of the embedded surface. In all cases, we consider$ \omega = 1 $ , which reduces to a traceless EMT, with$ T = 0 $ . See the text for specific choices of the considered parameters.$ \frac{\gamma r_0^2}{r^4} = \frac{8}{3} (\beta +3 \pi ) (p_r+2 p_t), $
(58) $ k(r) r \Phi '+ l(r) = -4 (\beta +6 \pi ) r^4 p_r+4 \beta r^4 p_t, $
(59) $\begin{aligned} k(r) r \Phi ''+6 r^2 (r-r_0) (r-\gamma r_0) \Phi '^2+3 r^2 (2 r-(\gamma +1) r_0) \Phi '+l(r) = -4 \beta r^4 p_r+ 4 (\beta +12 \pi ) r^4 p_t.\\\end{aligned} $
(60) Here,
$ k(r) = 6 r (r-r_0) (r-\gamma r_0) $ , and$ l(r) = 3 r_0 (\gamma r+r-\gamma r_0) $ . Eqs. (58) and (59) enable us to obtain explicit expressions for$ p_r $ and$ p_t $ in terms of b and$ b^{\prime} $ ,$ \begin{aligned}\\[-14pt]p_r = \frac{8 (\beta +3 \pi ) r (r-r_0) (r-\gamma r_0) \Phi '+\beta r_0 (5 \gamma r_0-4 (\gamma +1) r)-12 \pi r_0 (\gamma r+r-\gamma r_0)}{8 (\beta +3 \pi ) (\beta +4 \pi ) r^4}, \end{aligned}$
(61) $ p_t = \frac{r_0 (2 \beta (\gamma +1) r+6 \pi (\gamma +1) r-\beta \gamma r_0)-4 (\beta +3 \pi ) r (r-r_0) (r-\gamma r_0) \Phi '}{8 (\beta +3 \pi ) (\beta +4 \pi ) r^4}. $
(62) Inserting
$ p_r $ and$ p_t $ into Eq. (60), we obtain the following relationship:$ \begin{aligned}[b] & \Phi ' \left(4 r^2+2 r (r-r_0) (r-\gamma R) \Phi '-3 (\gamma +1) r r_0+2 \gamma r_0^2\right) \\&\qquad +2 r (r-r_0) (r-\gamma r_0) \Phi '' = \dfrac{(\beta +6 \pi ) \gamma r_0^2}{(\beta +3 \pi ) r}, \end{aligned} $
(63) which may be integrated to yield the solution
$ \Phi (r) = \log \left(\cos \left( \frac{\sqrt{2} {\cal{K}} \tanh ^{-1}\left( \dfrac{\sqrt{\gamma } \sqrt{r-r_0}}{\sqrt{r-\gamma r_0}} \right)}{\sqrt{\gamma } r_0}-k_1 \right)\right) + k_2 $
(64) where
$ {\cal{K}} = \sqrt{-\dfrac{(\beta +6 \pi ) \gamma r_0^2}{\beta +3 \pi }} $ , and$ k_1 $ and$ k_2 $ are integrating constants, which, at the throat, reduce to$ \Phi(r_0) = \ln \left(\cos \left(k_1\right)\right)+k_2. $
(65) At this juncture, we note a few considerations to maintain the regularity of the solution. We must impose
$ \cos\left(k_1\right) >0 $ so that$ \Phi(r) $ is finite at the throat. Interestingly, we find that the present case is similar to our previous case; thus, we do not repeat our discussion here. We may conclude that$ \Phi(r) $ given in Eq. (64) is finite as$ r\to \infty $ , which permits a horizonless solution.Inserting the redshift function (64) into expressions (61)–(62) and using Eq. (15), we finally have
$ \rho = \frac{3 \gamma r_0^2}{8 (\beta +3 \pi ) r^4}, $
(66) $ \rho+ p_r = \frac{4 \sqrt{2} (\beta +3 \pi ) r \sqrt{r-r_0} {\cal{M}}(r) +\beta r_0 (5 \gamma r_0-4 (\gamma +1) r)-12 \pi r_0 (\gamma r+r-\gamma r_0)}{8 (\beta +3 \pi ) (\beta +4 \pi ) r^4}, $
(67) $ \rho+p_t = \frac{r_0 (2 \beta (\gamma +1) r+6 \pi (\gamma +1) r-\beta \gamma r_0-2 \sqrt{2} (\beta +3 \pi ) {\cal{M}}(r) \sqrt{r-r_0}}{8 (\beta +3 \pi ) (\beta +4 \pi ) r^4}, $
(68) where
$ {\cal{M}}(r) = \sqrt{r-\gamma r_0} {\cal{K}} \tan \left( k_1 - \dfrac{\sqrt{2} {\cal{K}} \tanh ^{-1} \left(\dfrac{\sqrt{\gamma } \sqrt{r - r_0}}{\sqrt{r-\gamma r_0}}\right)}{\sqrt{\gamma } r_0} \right) $ . Having obtained the solutions for the matter fields, we plot ρ,$ \rho+p_r $ , and$ \rho+p_t $ in Fig. 8. It is important to emphasize that the region for the domain is$ -6 \pi<\beta < -3 \pi $ , where the WH is valid (see the expression for$ {\cal{K}} $ ). Note that$ \beta = -4\pi $ and$ \beta = -3 \pi $ are points of discontinuity where the solution is not valid. Fig. 8 depicts the behavior of the stress-energy components for$ -6 \pi<\beta < -3 \pi $ and$ \gamma = 0.5 $ . Observing the figure, we find that ρ and$ \rho+p_r $ are negative, whereas$ \rho+p_t $ is positive outside the throat, i.e.,$ r> r_0 = 1 $ . This clearly indicates that the NEC is violated outside the throat radius within the specified region.Figure 8. (color online) Here, we consider a specific shape function
$ b(r) = r_0+\gamma r_0 \left(1-\dfrac{r_0}{r}\right) $ and plots of the specific stress-energy profile for ρ (Left panel),$ \rho+p_r $ (Middle panel), and$ \rho+p_t $ (Right panel) versus r. In all cases, we consider$ \omega = 1 $ , which reduces to a traceless EMT, with$ T = 0 $ . See the text for specific choices of the considered parameters.The NEC at the throat is given by
$ (\rho+ p_r)|_{r_0} = \frac{\gamma -1}{2 (\beta +4 \pi ) r_0^2}, $
(69) $ (\rho+ p_t)|_{r_0} = \frac{2 \beta \gamma +\beta +\pi (9 \gamma +3)}{4 (\beta +3 \pi ) (\beta +4 \pi ) r_0^2}. $
(70) In this case,
$ (\rho+ p_{r})|_{r_0} <0 $ and$ (\rho+ p_{t})|_{r_0} \lessgtr 0 $ when$ -4 \pi<\beta < -3 \pi $ . Conversely,$ (\rho+ p_{r})|_{r_0} >0 $ and$(\rho+ p_{t})|_{r_0} < 0$ when$ -6 \pi<\beta < -4 \pi $ . Thus, it is clear that the NEC is always violated.Finally, we determine the total amount of exotic matter through the VIQ. Thus, using Eqs. (37) and (71), we obtain an approximate analytical solution for the definite integral with a cut-off of the stress-energy at
$ a>r_0 $ :$ \begin{aligned}\\[-5pt]I_V = \dfrac{1}{{48 (\beta +4 \pi ) \gamma ^{5/2} a^3 r_0^2}} \left[ \sqrt{\gamma } \left( \left(3 \gamma ^2 - 2 \gamma + 3\right) a^2 l_1 -8 \gamma ^2 r_0^2 \left(l_1 + 2 \gamma r_0^2\right) + 2 \gamma (\gamma +1) a r_0 \left(l_1 + 6 \gamma r_0^2\right)\right) - 3 \sqrt{2} (\gamma - 1)^2 (\gamma + 1) a^3 l_2 \right],\end{aligned} $ (71) where
$ l_1 = \sqrt{2}\sqrt{a-r_0} \sqrt{a-\gamma r_0} $ , and$ l_2 = \tanh ^{-1} \left(\dfrac{a-\sqrt{r-r_0} \sqrt{a-\gamma r_0}}{\sqrt{\gamma } r_0}\right) $ . Figure 9 is illustrated for$ \gamma = 0.5 $ ,$ k_1 = 1 $ , and varying β in the domain$ -6 \pi<\beta < -3 \pi $ , where the WH solution is valid. Observing Fig. 9 , we may infer that the amount of exotic matter can be made arbitrarily small through a judicious choice of the parameter space. -
To explore the deviation angle of photons from null geodesics, we begin by introducing a comprehensive line element that embodies both spherically symmetric and static characteristics [100, 101]. This line element can be represented as follows:
$ \mathrm{d}s^2 = -H(r) \mathrm{d}t^2 +G(r) \mathrm{d}r^2 +F(r) \mathrm{d}\Omega^2. $
(72) To characterize the trajectory of an object in free fall with respect to the underlying geometry [101], we make use of the geodesic equation. This equation establishes a relationship between the momentum one-forms of the object and the spacetime's geometry. It can be mathematically expressed as follows:
$ \frac{\mathrm{d}p_\beta}{\mathrm{d}\lambda} = \frac{1}{2} g_{\nu \alpha, \beta} p^\nu p^\alpha . $
(73) In this scenario, we assign the parameter λ to represent the affine parameter. It is important to emphasize that if the components of
$ g_{\alpha\nu} $ do not vary with respect to$ x^\beta $ for a fixed index β, then$ p_\beta $ remains constant throughout the motion. By exclusively considering the equatorial slice with$ \theta = \pi/2 $ , we discover that all the components$ g_{\alpha\beta} $ in Eq. (73) become independent of t, θ, and ϕ. As a result, we can identify the corresponding Killing vector fields$ \delta^{\mu}\alpha \partial\nu $ , with α as a cyclic coordinate. By designating the constants of motion as$ p_t $ and$ p_\phi $ , we can delve into the analysis of the system's dynamics using the following expressions:$ p_t = -E, \; \; \; \; \; \; \; \; \; \; p_\phi = L. $
(74) Here, E and L denote the energy and angular momentum of the photon, respectively. With this in mind, we can express the geodesic equation as
$ p_t = \dot{t} = g^{t \nu} p_\nu = \frac{E}{H(r)}, $
(75) $ p_\phi = \dot{\phi} = g^{\phi \nu} p_\nu = \frac{L}{F(r)}, $
(76) where the overdot notation represents differentiation with respect to the affine parameter λ. Continuing on from the previous analysis, we can straightforwardly obtain the radial null geodesic as
$ \dot{r}^2 = \frac{1}{G(r)} \left[ \frac{E^2}{H(r)} - \frac{L^2}{F(r)} \right]. $
(77) To provide a more precise formulation, we can express the equation for the photon trajectory in terms of the impact parameter
$ \mu = L/E $ as$ \left[ \frac{\mathrm{d}r}{\mathrm{d}\phi} \right]^2 = \frac{F(r)^2}{\mu^2 G(r)} \left[ \frac{1}{H(r)} - \frac{\mu^2}{F(r)} \right]. $
(78) Now, let us consider a photon source with radius
$ r_s $ that affects the underlying geometry. To determine the deflection angle of the photons, we must identify the conditions under which the photons can reach the surface. This occurs when a solution$ r_0 $ satisfies the conditions$ r_0 > r_s $ and$ \dot{r}^2 = 0 $ , where$ r_0 $ represents the distance of closest approach or the turning point. In this scenario, the impact parameter can be expressed as$ \mu = \frac{L}{E} = \pm \sqrt{\frac{F(r_0)}{H(r_0)}}, $
(79) In the regime of weak gravity, it becomes apparent that
$ \mu \approx \sqrt{{\cal{F}}(r_0)} $ . Therefore, if a photon originates from the polar coordinate limit defined as$ \lim\limits_{r \rightarrow \infty} \left( r, -\dfrac{\pi}{2}-\dfrac{\alpha}{2} \right) $ , passes through the turning point located at$ (r_0, 0) $ , and approaches$ \lim\limits_{r \rightarrow \infty} \left( r, \dfrac{\pi}{2}+\dfrac{\alpha}{2} \right) $ , we can define the deflection angle of the photon as α. This deflection angle, denoted by α, is dependent on$ r_0 $ [102] and can be explicitly derived from Eq. (79) as$ \alpha(r_0) = -\pi + 2 \int_{r_0}^{\infty} \sqrt{\frac{{\cal{G}}(r) }{{\cal{F}}(r)}}\left[ \left( \frac{{\cal{H}}(r_0)}{{\cal{H}}(r)} \right) \left( \frac{{\cal{F}}(r)}{{\cal{F}}(r_0)} \right) -1 \right]^{-1/2}\mathrm{d}r. $
(80) For the chosen metric coefficients in the
$ {\cal{WH}} $ geometry, we can now easily determine the deflection angle of photons in$ f(R, T) $ gravity by numerically integrating the formulas mentioned above, considering the shape functions specified by Eqs. b(r) =$r_0 \left(\dfrac{ 6\pi r+3 \pi r_0+ \beta r}{(\beta +9\pi)r }\right)^{{(3\pi+\beta)}/{(3\pi)}}$ ,$ b(r) = \dfrac{r_0^2}{r} $ , and$ b(r) = r_0+ \gamma r_0 \left(1-\dfrac{r_0}{r}\right) $ . Figure 10 shows the plots illustrating the phenomenon at hand. A negative deflection angle indicates the presence of repulsive gravity. To validate this phenomenon, we introduce the concept of the photon deflection angle on the WH. As stated in [103], in the presence of repulsive gravity acting on photons, the deflection angle becomes negative in the spacetime. Remarkably, the deflection angle consistently maintains negative values for all values of$ r_0 $ in the three solutions. This consistent negativity can be interpreted as a manifestation of the repulsive gravity effect.Figure 10. (color online) Behavior of the numerical results of the photon deflection angle, represented by the quantity
$ \alpha(r_0) $ , for three solutions. These plots demonstrate the negative deflection angle, indicating the repulsive nature of gravity in the three solutions. In all cases, we consider$ \omega = 1 $ , which reduces to a traceless EMT, with$ T = 0 $ . See the text for specific choices of the considered parameters.
Is dark energy necessary for the sustainability of traversable wormholes?
- Received Date: 2024-06-14
- Available Online: 2025-01-15
Abstract: Dark energy is typically the principal component needed for the traversability of wormholes (WH), as it provides the negative gravity effect required to keep the throat open. However, can this be achieved without dark energy? It turns out that if we couple the trace of energy-momentum with the standard Einstein-Hilbert Lagrangian and utilize a specific equation of state (EoS), dark energy may be obviated. The Casimir stress energy is known to result in the violation of the null energy condition (NEC) on the energy momentum tensor. This phenomenon makes such an EoS an ideal candidate for generating traversable WH geometries. The laboratory proven phenomenon provides a natural mechanism to sustain an open WH throat without relying on dark energy. Therefore, we generate two classes of WH solutions using this in energy-momentum trace-coupling gravity. For the specific choice of the Casimir EoS relating the energy-momentum tensor components [Kar and Sahdev: Phys. Rev. D 52, 2030 (1995)] and different choices of redshift functions, we determine the WH geometry completely. The obtained WH solutions violate the NECs, and all qualitative constraints demanded for physically realizable WHs are satisfied. This is demonstrated via graphical plots for a suitably chosen range of coupling parameter values. Furthermore, our study investigates the repulsive effect of gravity, revealing that its presence leads to a negative deflection angle for photons traveling along null geodesics. Notably, we observe a consistent pattern of negative values for the deflection angle across all values of