1 Introduction

Let us look at a process proceeding at tree level, depicted in Fig. 1, in which particle A decays into R and 1, and R further decays into particles 2 and 3. Triangle singularities stem from the related reaction mechanism, which is depicted in Fig. 2, where the particle A decays into R and 1, posteriorly R decays into 2 and 3 and later 1 and 2 fuse to give a new particle or simply rescatter to give the same state (or another one if there are inelasticities). Diagrammatically the process is depicted in Fig. 2 where there is a loop containing particles 1, 2 and R as intermediate states. This loop function can lead to some singularities (for the limit of zero width of the R particle) when all the three intermediate particles are placed on shell, particle 1 and 3 are antiparallel and furthermore a condition is fulfilled which in classical terms can be stated as corresponding to the decay of A at rest into R and 1, assuming R moves forward and 1 backward, then R decays into 2 and 3, and letting 3 go forward, 2 eventually goes backward, which means in the same direction of 1. If 2 moves faster than 1 it can catch it and either rescatter or fuse. These conditions are the essence of Coleman-Norton theorem [1]. Early studies of triangle singularities were done in Ref. [2] but the systematic study was done by Landau [3].

Work followed in Refs. [4,5,6,7] and some peaks observed in nuclear reactions [8] were suggested as indicative of a triangle singularity [9]. A thorough discussion of this early work was done by Schmid in a clarifying article [10]. There a surprise appeared, known nowadays as Schmid theorem that states that if the rescattering of particles 1 and 2 occurs, going to the same state \(1+2\), the triangle singularity does not lead to any observable effect in magnitudes like cross sections or differential widths. It is simply reabsorbed by the S-wave of the tree level amplitude (the same mechanism without rescattering, see Fig. 1) modifying only the phase of this partial amplitude. In angle-integrated cross sections the effect of the triangle singularity disappears.

Some debate originated on the limits to the Schmid theorem and its range of validity [11,12,13,14]. In Ref. [11], for example, it was shown that if the scattering amplitude of \(1+2 \rightarrow 1+2\) contains inelasticities then the Schmid theorem does not hold.

Recently there has been a renewed interest in triangle singularities because the present wealth of experimental work offers multiple possibilities to study such mechanisms. A topic that stimulated the present interest on the subject was the one of isospin violation in the \(\eta (1405)\) decay into \(\pi ^0 f_0(980)\) versus the isospin allowed decay into \(\pi ^0 a_0(980)\) [15,16,17,18,19]. One interesting work was done in Ref. [20], with many suggestions of places and reactions where triangle singularities could be found. One of the most striking examples of this rebirth is the work of Refs. [21, 22] where a peak observed by the COMPASS collaboration [23], and branded as a new resonance \(a_1(1420)\), was shown to be actually produced by a triangle singularity. The renewed interest in the issue was also spurred by the work of Ref. [24], suggesting that a peak observed by the LHCb collaboration, which has been accepted as a signal of a pentaquark of hidden charm [25], was actually due to a triangle singularity. The hypothesis was ruled out in Ref. [26] if the present quantum numbers of this peak hold. Yet, given the fact that some uncertainties concerning these quantum numbers still remain, the issue could be reopened in the future.

The work of Ref. [26] develops a different formalism than the one usually employed, which is very practical and intuitive, and we shall also follow these lines in the present work, which offers a quite different formal derivation of Schmid theorem and allows to see its validity and limitations.

The former recent works on triangle singularities have stimulated many works on the issue [27,28,29,30,31,32,33,34,35,36,37,38,39,40,41,42,43,44,45,46]. Further information can be found in the report [47].

Along the literature on this topic it is customary to find the statement that due to the Schmid theorem, whenever one has rescattering in the loop to go to the same states as inside the loop, there is no need to evaluate the triangle diagram because its contribution is reabsorbed by the tree level. The purpose of the present paper is to get an insight on the theorem and see where it holds exactly, when it fails and when it is just an approximation and how good or bad can it be. For that, a new derivation is carried out, and a study in terms of the width of the intermediate state R is done. The failure of the theorem when the \(t_{12,12}\) scattering matrix has inelasticities is also shown in detail, providing the quantitative amount of the breaking of the theorem. Apart from the limit of small \(\Gamma _R\), where the theorem strictly holds, we study in a particular case what happens for a realistic width, and a typical \(1+2 \rightarrow 1+2\) scattering amplitude, which serves as a guide on how much to trust the theorem to eventually neglect the contribution of the triangle loop.

2 Formulation

Let us study the decay process of a particle A into two particles 1 and R, with a posterior decay of R into particles 2 and 3. This is depicted in Fig. 1.

Fig. 1
figure 1

Tree level diagram for the process \(A \rightarrow 1 +2 +3\) mediated by a resonance R that decays into particles 2 and 3. In brackets the momenta of the particles

We shall also assume for simplicity that all vertices are scalar, and can be represented by just one coupling in each vertex. The conclusions that we will reach are the same for more elaborate couplings, with spin or momentum dependence.

The next step is to allow particles 1 and 2 to undergo final state interaction, as depicted in Fig. 2.

Fig. 2
figure 2

Triangle mechanism emerging from the mechanism of Fig. 1, with final state interaction of particles 1 and 2. In brackets the momenta of the particles

The vertex with particles 1 and 2 symbolizes the \(1+2 \rightarrow 1+2\) scattering matrix. One peculiar property of triangle diagrams is that they can develop a singularity when all the particles inside the loop in Fig. 2 are placed on shell in the integration and the particles R and 3 go parallel in the A rest frame [3]. The conditions for this to occur, relating the invariant mass of particles 1, 2 with the mass of A, can be seen in a pedagogical description of the process in Ref. [26]. It is interesting to note that if particles R and 3 go in the same direction, then both particles 1 and 2 go in the opposite direction to them in the A and R rest frames, respectively. According to the Coleman-Norton theorem [1] the singularity appears when the classical process of particle 2, moving in the same direction as particle 1, but produced later, catches up with particle 1 and scatters (or fuse to produce another particle).

One should note that in the situation where the R resonance is placed on shell in the triangle loop, as well as particles 1 and 2, the tree level mechanism of Fig. 1 will also have a singularity in the limit of zero width for the resonance R, since the amplitude goes as \((M_\mathrm{inv}(R) -M_R +i\Gamma _R/2)^{-1}\). However, the tree diagram does not have the restriction that particles R and 3 should be parallel and hence the region where R can be placed on shell is much wider than for the triangle singularity.

Let us come back to the tree level mechanism of Fig. 1. Assume for the moment that the decay into \(2+3\) is the only decay channel of the resonance R. In the limit of \(\Gamma _R \rightarrow 0\) one has the decay of A into two elementary particles 1 and R. The width of A can be calculated with the standard formula for decay of two particles or three particles and the results are identical. Intuitively one can say that, once the particle decays into 1 and R, if particle R decays later this does not modify the A width, since this was determined at the moment that A decayed into 1 and R. The same could be said about the triangle mechanism of Fig. 2. Once the A particle decays into 1 and R, and R decays into 2 and 3, the probability for this process is established and the posterior interaction of 1 and 2 should not modify this probability. This argument is the intuitive statement of the Schmid theorem, which technically reads as follow: Let \(t_t^{(0)}\) be the S-wave projection of the tree level amplitude, \(t_t\), of the diagram of Fig. 1, evaluated in the rest frame of \(1+2\), referred to the angle between the particles 1 and 3. Let \(t_L\) be the amplitude corresponding to the triangle loop of Fig. 2. The Schmid theorem states that

$$\begin{aligned} t_t^{(0)} +t_L = t_t^{(0)}e^{2i\delta }, \end{aligned}$$
(1)

where \(\delta \) is the S-wave phase shift of the scattering amplitude \(1+2 \rightarrow 1+2\) (assume also for simplicity that this is the only partial wave in \(1+2 \rightarrow 1+2\)). The formula holds for the case that there is only elastic scattering \(1+2 \rightarrow 1+2\). In the case that there can be inelastic channels the formula is modified, as we shall see later on, and the Schmid theorem does not strictly hold.

The interesting thing about Eq. (1) is that

$$\begin{aligned} \left| t_t^{(0)}+t_L\right| ^2 = \left| t_t^{(0)}e^{2i\delta }\right| ^2 = \left| t_t^{(0)}\right| ^2, \end{aligned}$$
(2)

and consequently, since \(t_t^{(\ell \ne 0)}\) and \(t_t^{(0)}\) do not interfere in the angle integration, then

$$\begin{aligned} \int _{-1}^{1} d\cos \theta \left| t_t +t_L\right| ^2&= \int _{-1}^{1} d\cos \theta \left| t_t^{(\ell \ne 0)} +t_t^{(0)} +t_L\right| ^2 \nonumber \\&= \int _{-1}^{1} d\cos \theta \left| t_t^{(\ell \ne 0)} +t_t^{(0)}e^{2i\delta }\right| ^2 \nonumber \\&= \int _{-1}^{1} d\cos \theta \left( |t_t^{(\ell \ne 0)}|^2 +|t_t^{(0)}|^2\right) \nonumber \\&= \int _{-1}^{1} d\cos \theta |t_t|^2, \end{aligned}$$
(3)

and as a consequence the contribution of the triangle diagram does not change the width that one obtains just with the tree level diagram. Note that if we had \(1+2 \rightarrow 1^\prime +2^\prime \) or \(1+2 \rightarrow R^\prime \), where \(R^\prime \) is some resonance, the theorem does not hold because there is no contribution of the tree level to these reactions.

2.1 Kinematics of \(A \rightarrow 1+2+3\)

We assume that all particles are mesons to avoid using different normalization for meson or baryon fields. The width of particle A for this process is given by

$$\begin{aligned} \Gamma _A&= \frac{1}{2M_A} \int \frac{d^3p_3}{(2\pi )^3}\frac{1}{2\omega _3} \int \frac{d^3p_2}{(2\pi )^3}\frac{1}{2\omega _2} \int \frac{d^3p_1}{(2\pi )^3}\frac{1}{2\omega _1}\nonumber \\&\quad \times (2\pi )^4\delta ^4(P_A -p_1 -p_2 -p_3) \,|t|^2, \end{aligned}$$
(4)

where \(P_A\) is the four-momentum of A and \(\omega _i\) the on shell energies \(\omega _i = \sqrt{m_i^2 + \vec {p_i}^2}\). We perform the integration over particles 1 and 2 in the frame of reference where \(\vec {P}_A -\vec {p}_3=0\), where the system of \(1+2\) is at rest and the integration over \(p_3\) in the A rest frame. We perform the \(d^3p_2\) integration using the \(\delta \) function and have in that frame (\(\vec {p}_2=-\vec {p}_1\))

$$\begin{aligned} \Gamma _A&= \frac{1}{2M_A} \int \frac{d^3p_3}{(2\pi )^3}\frac{1}{2\omega _3} \int \frac{d^3\widetilde{p}_1}{(2\pi )^3} \frac{1}{2\widetilde{\omega }_1} \frac{1}{2\widetilde{\omega }_2}\nonumber \\&\quad \times 2\pi \delta \left( \widetilde{E}_A -\widetilde{\omega }_3 -\widetilde{\omega }_1(\widetilde{p}_1) -\widetilde{\omega }_2(\widetilde{p}_1)\right) \,|t|^2, \end{aligned}$$
(5)

where the tilde refers to variables in the \(1+2\) rest frame, and t is the scattering matrix for the process.

Note that

$$\begin{aligned} \widetilde{E}_A -\widetilde{\omega }_3 =\widetilde{\omega }_1(\widetilde{p}_1) +\widetilde{\omega }_2(\widetilde{p}_1) = M_\mathrm{inv}(12). \end{aligned}$$
(6)

There is no \(\phi \) dependence in that frame if we chose \(\vec {\widetilde{p}_3}\) in the z direction and the \(d^3\widetilde{p}_1\) integration is done with the result

$$\begin{aligned} \Gamma _A = \frac{1}{2M_A} \int \frac{d^3p_3}{(2\pi )^3}\frac{1}{2\omega _3} \frac{1}{8\pi } \int _{-1}^{1}d\cos \theta \, \widetilde{p}_1 \frac{1}{M_\mathrm{inv}(12)} \,|t|^2, \end{aligned}$$
(7)

with \(\widetilde{p}_1\) the momentum of particle 1 in the \(1+2\) rest frame and \(\theta \) the angle between \(\vec {\widetilde{p}_1}\) and \(\vec {\widetilde{p}_3}\).

Note also that

$$\begin{aligned} M_\mathrm{inv}^2(23) = (P_A -p_1)^2 = M_A^2 +m_1^2 -2\widetilde{E}_A\widetilde{E}_1 +2\widetilde{p}_1\widetilde{p}_3\cos \theta . \end{aligned}$$
(8)

Hence, the integration over \(\cos \theta \) is equivalent to an integration over \(M_\mathrm{inv}(23)\). Similarly we can write

$$\begin{aligned} M_\mathrm{inv}^2(12) = (P_A -p_3)^2 = M_A^2 +m_3^2 -2M_A\omega _3, \end{aligned}$$
(9)

where the evaluation has been done in the A rest frame. It is also easy to derive.

$$\begin{aligned} \widetilde{E}_A&= \frac{1}{2M_\mathrm{inv}(12)}\left( M_A^2 + M_\mathrm{inv}^2(12) -m_3^2\right) \nonumber \\ \widetilde{E}_3&= \frac{1}{2M_\mathrm{inv}(12)}\left( M_A^2 - M_\mathrm{inv}^2(12) -m_3^2\right) \nonumber \\ \widetilde{E}_1&= \frac{1}{2M_\mathrm{inv}(12)}\left( M_\mathrm{inv}^2(12) +m_1^2 -m_2^2\right) \nonumber \\ \widetilde{p}_1&= \frac{\lambda ^{1/2}\left( M_\mathrm{inv}^2(12),m_1^2,m_2^2\right) }{2M_\mathrm{inv}(12)} \nonumber \\ \widetilde{p}_3&= \frac{\lambda ^{1/2}\left( M_A^2,m_3^2,M_\mathrm{inv}^2(12)\right) }{2M_\mathrm{inv}(12)}. \end{aligned}$$
(10)

The \(d^3p_3\) integration is done in the A rest frame

$$\begin{aligned} \int \frac{d^3p_3}{(2\pi )^3}\frac{1}{2\omega _3} = \frac{1}{4\pi ^2} \int p_3 \, d\omega _3, \end{aligned}$$
(11)

and using Eqs. (8) and (9), the \(\omega _3\) and \(\cos \theta \) integration can be substituted by integrations over \(M_\mathrm{inv}(12)\) and \(M_\mathrm{inv}(23)\) and one has the formula given in the PDG [48]

$$\begin{aligned} \frac{d^2\Gamma _A}{dM_\mathrm{inv}(12)dM_\mathrm{inv}(23)} = \frac{1}{64\pi ^3}\frac{1}{M_A^3} M_\mathrm{inv}(12)M_\mathrm{inv}(23) \,|t|^2. \end{aligned}$$
(12)

Yet, for the explanation of the Schmid theorem it is better to use Eq. (7).

2.2 \(t_t\) and \(t_L\) amplitudes

Since we are concerned only with the situation when the particles are close to on shell we will use

$$\begin{aligned}&\frac{1}{q^2 -m^2 +i\epsilon } = \frac{1}{(q^0)^2 -\vec {q\,}^2 -m^2 +i\epsilon } \nonumber \\&= \frac{1}{2\omega (q)}\left\{ \frac{1}{q^0 -\omega (q) +i\epsilon } - \frac{1}{q^0 +\omega (q) +i\epsilon }\right\} , \end{aligned}$$
(13)

and keep only the term \(\left[ 2\omega (q)\left( q^0 -\omega (q) +i\epsilon \right) \right] ^{-1}\) since this is the term that can be placed on shell.

The amplitude of Fig. 1 is given in the \(1+2\) rest frame by (\(\vec {P}_A = \vec {p}_3\), and we omit the tilde in the momenta)

$$\begin{aligned} t_t = g_A \, g_R \, \frac{1}{2\omega _R(\vec {p}_3 -\vec {q}\,)}\frac{1}{\widetilde{E}_A -\omega _1(q) -\omega _R(\vec {p}_3 -\vec {q}\,) +i\epsilon }, \end{aligned}$$
(14)

where \(g_A, \, g_R\) are the couplings for the decay of A and R. From Eq. (14) we get \(t_t^{(0)}\) projecting into S-wave

$$\begin{aligned} t_t^{(0)}&= \frac{1}{2}\int _{-1}^{1}d\cos \theta \frac{1}{2\omega _R(\vec {p}_3 -\vec {q}\,)}\nonumber \\&\quad \times \frac{g_A \, g_R}{\widetilde{E}_A -\omega _1(q) -\omega _R(\vec {p}_3 -\vec {q}\,) +i\epsilon }. \end{aligned}$$
(15)

Note that in the realistic situation the \(i\epsilon \) in Eqs. (14) and (15) will be substituted by \( i\frac{\Gamma _R}{2}\).

On the other hand, the amplitude of the triangle diagram can be written in the \(1+2\) rest frame as

$$\begin{aligned} t_L&= i\int \frac{d^4q}{(2\pi )^4} \, \frac{1}{2\omega _R(\vec {p}_3 -\vec {q}\,)} \, \frac{1}{\widetilde{E}_A -q^0 -\omega _R(\vec {p}_3 -\vec {q}\,) +i\epsilon }\nonumber \\&\quad \times \,\frac{1}{2\omega _1(q)} \, \frac{1}{q^0 -\omega _1(q) +i\epsilon } \, \frac{1}{2\omega _2(q)}\nonumber \\&\quad \times \frac{1}{\widetilde{E}_A -q^0 -\widetilde{E}_3 -\omega _2(q) +i\epsilon }\, g_A \, g_R \, t_{12,12}, \end{aligned}$$
(16)

where \(t_{12,12}\) is the scattering amplitude for \(1+2 \rightarrow 1+2\). The \(q^0\) integration is done immediately using Cauchy’s theorem and we obtain

$$\begin{aligned} t_L&= \int \frac{d^3q}{(2\pi )^3} \, \frac{1}{2\omega _R(\vec {p}_3 -\vec {q}\,)} \, \frac{1}{\widetilde{E}_A -\omega _1(q) -\omega _R(\vec {p}_3 -\vec {q}\,) +i\epsilon }\nonumber \\&\quad \times \frac{1}{2\omega _1(q)} \, \frac{1}{2\omega _2(q)} \, \frac{g_A \, g_R \, t_{12,12}}{\widetilde{E}_A -\omega _1(q) -\widetilde{E}_3 -\omega _2(q) +i\epsilon }. \end{aligned}$$
(17)

We can see that the R propagator term \(\big [ 2\omega _R(\vec {p}_3 -\vec {q}\,) \left( \widetilde{E}_A -\omega _1(q) -\omega _R(\vec {p}_3 -\vec {q}\,) +i\epsilon \right) \big ]^{-1}\) is common in \(t_t\) and \(t_L\) of Eqs. (14) and (17). There is, however, a difference since in the loop function \(t_L\) the momentum \(\vec {q}\) is an integration variable while, in \(t_t\), \(\vec {q}\) is the momentum of the external particle 1. In the loop, after rescattering of particles 1 and 2 the momentum \(\vec {p}_1\) is different than \(\vec {q}\), and only for the situation where all particles in the loop are placed on shell, the moduli of the momenta are equal.

The \(\phi \) integral in Eq. (17) is trivially done and we have

$$\begin{aligned} t_L&= \frac{1}{(2\pi )^2}\int _0^\infty q^2\, dq \, \frac{1}{2\omega _1(q)} \, \frac{1}{2\omega _2(q)}\nonumber \\&\quad \times \frac{1}{\widetilde{E}_A -\widetilde{E}_3 -\omega _1(q) -\omega _2(q) +i\epsilon }\nonumber \\&\quad \times \, 2\, \frac{1}{2} \int _{-1}^{1}d\cos \theta \, \frac{1}{2\omega _R(\vec {p}_3 -\vec {q}\,)}\nonumber \\&\quad \times \frac{1}{\widetilde{E}_A -\omega _1(q) -\omega _R(\vec {p}_3 -\vec {q}\,) +i\epsilon } \, g_A \, g_R \, t_{12,12}. \end{aligned}$$
(18)

We can see now that the integral over \(\cos \theta \) is the same in \(t_t^{(0)}\) (Eq. (15)) and \(t_L\) (Eq. (18)).

To find the singularity in \(t_L\) let us look for the poles of the two propagators. On the one hand from

$$\begin{aligned} \widetilde{E}_A -\widetilde{E}_3 -\omega _1(q) -\omega _2(q) +i\epsilon =0, \end{aligned}$$
(19)

we obtain

$$\begin{aligned} q_\mathrm{on \, \pm } = \pm \frac{\lambda ^{1/2}\left( M_\mathrm{inv}^2(12),m_1^2,m_2^2\right) }{2M_\mathrm{inv}(12)} \pm i\epsilon . \end{aligned}$$
(20)

On the other hand from

$$\begin{aligned} \widetilde{E}_A -\omega _1(q) -\omega _R(\vec {p}_3 -\vec {q}\,) +i\epsilon =0, \end{aligned}$$
(21)

we get two solutions which depend on \(\cos \theta \). Yet we are only interested in \(\cos \theta = \pm 1\) because it is there that we will not have cancellations in the principal value of \( \int _{-1}^{1}d\cos \theta \) because we cannot go beyond \(|\cos \theta \,|=1\) in the integration. In this case one finds immediatelyFootnote 1

$$\begin{aligned} \overline{q} = p_3\cos \theta \frac{E_1^\prime }{M_A} \pm \frac{\widetilde{E}_A}{M_A}p_1^\prime \pm i \epsilon , \quad (\cos \theta = \pm 1), \end{aligned}$$
(22)

where \(E_1^\prime , \, p_1^\prime \) are the energy and momentum of particle 1 in the A rest frame, while \(p_3\) is the momentum of particle 3 (or A) in the \(1+2\) rest frame that we have used before. For \(\cos \theta = \pm 1\) this is just a boost from the frame where A is at rest (\(\overline{q} = p_1^\prime \)) to the one where it has a velocity \( v_A = \frac{\widetilde{p}_A}{\widetilde{E}_A} = \frac{p_3}{\widetilde{E}_A}\), but the position in the complex plane is given by the \(\pm i \epsilon \).

Take now:

  1. (a)

    \(\cos \theta = -1\)

The \((-)\) solution in Eq. (22),

$$\begin{aligned} Q_- = -p_3\frac{E_1^\prime }{M_A} - \frac{\widetilde{E}_A}{M_A}p_1^\prime - i \epsilon , \end{aligned}$$
(23)

gives \(\overline{q}\) negative and does not contribute in Eq. (18) since q runs from 0 to \(\infty \). If we take the \((+)\) sign,

$$\begin{aligned} Q_+ = -p_3\frac{E_1^\prime }{M_A} +\frac{\widetilde{E}_A}{M_A}p_1^\prime + i \epsilon , \end{aligned}$$
(24)
Fig. 3
figure 3

Pole positions for the case of \(\cos \theta = -1\) when \(\overline{q}\) can be positive. The line shows the contour path that one can take to avoid the poles

the pole is in the upper side of the complex plane. This situation corresponds to the one in Fig. 3. We can see that in that case one can deform the contour path in the q integration to avoid the poles and one does not have a singularity.

  1. (b)

    \(\cos \theta = 1\)

The \((+)\) solution,

$$\begin{aligned} q_\mathrm{a +} = p_3 \frac{E_1^\prime }{M_A} + \frac{\widetilde{E}_A}{M_A}p_1^\prime +i \epsilon , \end{aligned}$$
(25)

corresponds to a pole in the upper part of the complex plane and does not lead to a singularity. The \((-)\) solution, let us call it \(q_\mathrm{a -}\),

$$\begin{aligned} q_\mathrm{a -} = p_3 \frac{E_1^\prime }{M_A} - \frac{\widetilde{E}_A}{M_A}p_1^\prime -i \epsilon , \end{aligned}$$
(26)

lies in the lower side of the complex plane. In this case if \(q_\mathrm{a -}\) is different from \(q_\mathrm{on}\) of Eq. (20) we have the situation as in Fig. 4a. In this case we can also deform the contour path to avoid the poles in the q integration of \(t_L\).

Fig. 4
figure 4

Pole positions for \(q_\mathrm{on}\) and \(q_\mathrm{a -}\) for \(\cos \theta = 1\). The case (b) leads to the triangle singularity

However in the case that

$$\begin{aligned} q_\mathrm{on+} = q_\mathrm{a -} \qquad (\epsilon \rightarrow 0), \end{aligned}$$
(27)

corresponding to Fig. 4b, the path of the integral has to go through the poles \(q_\mathrm{on+}\) and \(q_\mathrm{a-}\) and we cannot deform the contour path to avoid the poles. This is the situation of the triangle singularity.Footnote 2 Note for further discussions that \(Q_- = -q_\mathrm{a +}\) and \(Q_+ = -q_\mathrm{a -}\).

It might be curious to see that we find the singularity for \(\cos \theta = 1\), while in Ref. [26] it was found for \(\cos \theta = -1\). This is a consequence of the different frame of reference. Indeed, we are in the situation of Fig. 5.

We can make a boost with velocity \(v_A\) to bring particle A at rest

$$\begin{aligned} v_A = \frac{\widetilde{p}_A}{\widetilde{E}_A} = \frac{p_3}{\widetilde{E}_A}. \end{aligned}$$
(28)

The velocity of particle 3 in the \(1+2\) rest frame is

$$\begin{aligned} v_3 = \frac{p_3}{\widetilde{E}_3} > v_A, \end{aligned}$$
(29)

but since the mass of particle 3 is smaller than \(M_A\) then \(v_3\) is bigger than \(v_A\) and in the boost particle 3 still goes in the same direction as before. However \(p_1^\prime \) in that frame has a velocity

$$\begin{aligned} v_1 = \frac{p_1^\prime }{E_1^\prime }, \end{aligned}$$
(30)

and since we are taking the \(q_\mathrm{a-}\) solution positive

$$\begin{aligned}&q_\mathrm{a-} = p_3 \frac{E_1^\prime }{M_A} - \frac{\widetilde{E}_A}{M_A}p_1^\prime> 0 \, ,\nonumber \\&p_3E_1^\prime> p_1^\prime \widetilde{E}_A \, ; \qquad \frac{p_3}{\widetilde{E}_A}> \frac{p_1^\prime }{E_1^\prime } \Rightarrow v_A \,>\, v_1 \, . \end{aligned}$$
(31)

Hence particle 1 changes direction under the boost of velocity \(v_A\) and in the rest frame \(\vec {p_3}^\prime \) and \(\vec {p_1}^\prime \) have opposite directions, \(\cos \theta ^\prime = -1\), as it was found in Ref. [26].

Fig. 5
figure 5

Situation of momenta in the \(1+2\) rest frame when \(\cos \theta = 1\)

Fig. 6
figure 6

Integration path followed to evaluate \(t_L\) of Eq. (35)

2.3 Formulation of Schmid theorem

Let us perform the \(\cos \theta \) integration in \(t_L\) of Eq. (18).

$$\begin{aligned} I(q)&= \int _{-1}^{1} d \cos \theta \, \frac{1}{2\omega _R(\vec {p}_3 -\vec {q})} \nonumber \\&\quad \times \, \frac{1}{\widetilde{E}_A -\omega _1(q) -\omega _R(\vec {p}_3 -\vec {q}) +i\epsilon }. \end{aligned}$$
(32)

We can introduce the variable x

$$\begin{aligned} x&= \omega _R(\vec {p}_3 -\vec {q}) = \sqrt{m_R^2 + p_3^2 +q^2 -2p_3q\cos \theta } \nonumber \\ d\cos \theta&= -\frac{\omega _R}{p_3 q} dx \end{aligned}$$
(33)
$$\begin{aligned} I(q)&= -\int _{\omega _R(p_3 +q)}^{\omega _R(p_3 -q)} d\,x\,\frac{1}{2\omega _R}\,\frac{\omega _R}{p_3q}\, \frac{1}{\widetilde{E}_A -\omega _1(q) -x +i\epsilon }\nonumber \\&= \int _{\omega _R(p_3 -q)}^{\omega _R(p_3 +q)}\, d\,x\,\frac{1}{2p_3q}\,\frac{1}{\widetilde{E}_A -\omega _1(q) -x +i\epsilon }\nonumber \\&= \frac{1}{2p_3q}\ln \left( \frac{\widetilde{E}_A -\omega _1(q) -\omega _R(p_3 -q) +i\epsilon }{\widetilde{E}_A -\omega _1(q) -\omega _R(p_3 +q) +i\epsilon }\right) \, . \end{aligned}$$
(34)

It is interesting to see that \(I(q)=I(-q)\) is an even function of q. Then, since the rest of the integrand of \(t_L\) in Eq. (18) is also even in q we can write

$$\begin{aligned} t_L&= \frac{1}{(2\pi )^2}\frac{1}{2}\int _{-\infty }^{\infty } q^2\, dq\, \frac{1}{2\omega _1(q)}\,\frac{1}{2\omega _2(q)}\nonumber \\&\quad \times \,\frac{g_A \, g_R \, I(q) \, t_{12,12}}{\widetilde{E}_A -\widetilde{E}_3 -\omega _1(q) -\omega _2(q) +i\epsilon }\, . \end{aligned}$$
(35)

We should note that the singularity that we are evaluating corresponds to the numerator in Eq. (34) becoming zero.

Since we have extended the integration to q negative, we must also consider the poles of \(Q_-\) and \(Q_+\) of Eqs. (23) and (24). The situation of the poles is shown in Fig. 6.

In this figure we also show the contour path followed to perform the integral over q using Cauchy’s theorem. We have

$$\begin{aligned}&\int _{-\infty }^{\infty } dq \,\dots + \int _{i\infty }^{-i\infty } dq \,\dots + \int _\mathrm{circle} dq \,\dots \nonumber \\&\quad = 2\pi i \,\mathrm{Res}(q_\mathrm{on +}) + 2\pi i \,\mathrm{Res}(q_\mathrm{a +}) \end{aligned}$$
(36)
$$\begin{aligned}&\qquad - 2\pi i \,\mathrm{Res}(q_\mathrm{on -}) - 2\pi i \,\mathrm{Res}(Q_-) \end{aligned}$$
(37)

The relevant point now is the fact that the integral over the circle of infinity vanishes and \( \int _{i\infty }^{-i\infty } dq\), \(\mathrm{Res}(q_\mathrm{a +})\) and \(\mathrm{Res}(Q_-)\) do not produce any singularity, and thus

$$\begin{aligned} \int _{-\infty }^{\infty } dq \,\dots = 2\pi i \,\mathrm{Res}(q_\mathrm{on +}) - 2\pi i \,\mathrm{Res}(q_\mathrm{on -}), \end{aligned}$$
(38)

is the part of the integral that leads to the singularity. We go back to Eq. (18) and perform the q integration before \(\cos \theta \) is integrated. Since the denominator \(\left( \widetilde{E}_A -\widetilde{E}_3 -\omega _1(q) -\omega _2(q)\right) \) vanishes for \(q_\mathrm{on +}\) and \(q_\mathrm{on -}\), we can apply L’Hôpital rule to calculate the residues (\(\widetilde{E}_A -\widetilde{E}_3 = M_\mathrm{inv}(12)\), with \(q_\mathrm{on}\) standing for \(q_\mathrm{on +}\) or \(q_\mathrm{on -}\))

$$\begin{aligned} \mathrm{Res}(q_\mathrm{on})&\propto \lim _{q\rightarrow q_\mathrm{on}} \frac{q -q_\mathrm{on}}{M_\mathrm{inv}(12) -\omega _1(q) -\omega _2(q)}\nonumber \\&= \frac{1}{\left( \frac{-q}{\omega _1}\right) +\left( \frac{-q}{\omega _2}\right) } \Bigg |_{q_\mathrm{on }} = -\frac{\omega _1\,\omega _2}{q_\mathrm{on}\,M_\mathrm{inv}(12)}. \end{aligned}$$
(39)

Thus, the singular part of \(t_L\) is contained in

$$\begin{aligned} t_L&= \frac{1}{(2\pi )^2}\,\frac{1}{4}\,|q_\mathrm{on}|\,\frac{1}{M_\mathrm{inv}(12)}\, g_A\, g_R\, t_{12,12}\,(-)4\pi i \nonumber \\&\quad \times \, \frac{1}{2} \int _{-1}^{1}d\cos \theta \, \frac{1}{2\omega _R(\vec {p}_3 -\vec {q}\,)}\nonumber \\&\quad \times \,\frac{1}{\widetilde{E}_A -\omega _1(q) -\omega _R(\vec {p}_3 -\vec {q}\,) +i\epsilon }. \end{aligned}$$
(40)

Comparing with Eq. (15) we find

$$\begin{aligned} t_L = -i \, \frac{1}{4\pi }\,|q_\mathrm{on}|\,\frac{1}{M_\mathrm{inv}(12)}\,t_{12,12}\,t_t^{(0)}. \end{aligned}$$
(41)

We must now recall the relationship of our t matrix in the field theory formulation with the f matrix of Quantum Mechanics

$$\begin{aligned} f = - \frac{1}{8\pi }\,\frac{1}{M_\mathrm{inv}}\,t, \end{aligned}$$
(42)

which allows us to reformulate Eq. (41) as

$$\begin{aligned} t_L = 2\, i\, |q_\mathrm{on}| \, f \, t_t^{(0)}, \end{aligned}$$
(43)

and since

$$\begin{aligned} f = \frac{\eta \, e^{2i\delta } -1}{2 \, i \, |q_\mathrm{on}|}, \end{aligned}$$
(44)

we find that

$$\begin{aligned} t_t^{(0)} +t_L = t_t^{(0)}(1 +2 \, i \, |q_\mathrm{on}| \, f) = \eta \, e^{2i\delta }\, t_t^{(0)}, \end{aligned}$$
(45)

also derived in Ref. [14]. Eq. (45) for the case when there is only the 1, 2 elastic channel (\(\eta =1\)) is the expression of the Schmid theorem [10]. It was already mentioned in Ref. [11] that the Schmid theorem does not hold if \(t_{12,12}\) has inelasticities and we can be more quantitative here. Indeed, recalling Eq. (3) we have now

$$\begin{aligned}&\int _{-1}^{1} d\cos \theta \left| t_t +t_L\right| ^2 = \int _{-1}^{1} d\cos \theta \left\{ \left| t_t^{(\ell \ne 0)}\right| ^2 +\eta ^2\left| t_t^{(0)}\right| ^2\right\} \nonumber \\&\quad = \int _{-1}^{1} d\cos \theta \left\{ \left| t_t^{(\ell \ne 0)}\right| ^2 +\left| t_t^{(0)}\right| ^2 -(1-\eta ^2)\left| t_t^{(0)}\right| ^2 \right\} \nonumber \\&\quad = \int _{-1}^{1} d\cos \theta \left| t_t\right| ^2 \; -(1-\eta ^2) \int _{-1}^{1} d\cos \theta \left| t_t^{(0)}\right| ^2 \end{aligned}$$
(46)

and since \(t_t^{(0)}\) contains the same singularity as \(t_L\), the singularity of the triangle diagram will show up with a strength of \(1-\eta ^2\).

It is interesting to recall at this point that Watson’s theorem [49] does not hold in this case. We might expect that the sum of the tree level and rescattering would introduce a phase \(e^{i\delta }\) in the final state for elastic rescattering, while we see that in the present case one introduces the phase \(e^{i2\delta }\) on top of \(t_t^{(0)}\), which is itself complex from the structure of the R propagator. A detailed discussion of this issue can be found in Ref. [12].

It is also interesting to mention the effects of further rescattering beyond our triangle diagram. Final state interaction with three particles in the final state has been addressed repeatedly. One of the early works on this issue concerns rescattering in the \(K\rightarrow 3\pi \) decay [50] (for a modern reformulation of this problem one can see the work of Ref. [51]). What is relevant for our problem is that further rescattering of particles 1, 2 in Fig. 2 is already accounted for by the \(t_{12,12}\) scattering matrix that sums all the rescattering loops implicit in the Lippmann-Schwinger equation that generates \(t_{12,12}\). However, after the mechanism of Fig. 2 one can have for instance, rescattering of particles 2 and 3 which would lead to a new loop with the former external 2 and 3 particles now being intermediate particles. Note that then particles 2 and 3 in the new loop could be off shell, in which case the triangle singularity of the 1R2 triangle would be destroyed. Even if one concentrates on the contribution of 2 and 3 on shell in the loop, there is an angle integration for \(p_3\), and \(p_3\) of the new loop and q would no longer be parallel in the whole range of the \(p_3\) integration, which was a necessary condition for the triangle singularity. Hence, this new rescattering term would not have the triangle singularity structure and would be a smooth background term. Nevertheless, the modern techniques [51] allow to calculate such terms if precision is desired in a physical process. Yet, these issues go beyond the problem at hand, which is the investigation of the triangle mechanism, to which we come back.

3 Study of the singular behavior

Let us look at the behavior of \(t_L\) around the triangle singularity. For this it is easier to look at \(t_t^{(0)}\) which has this same singularity. Let us look at Eq. (15). The integral there is \( \frac{1}{2} I(q) g_A g_R\), with I(q) from Eq. (34). Hence

$$\begin{aligned} t_t^{(0)} =\frac{g_A \, g_R}{4 p_3 \, q}\, \ln \left( \frac{\widetilde{E}_A -\omega _1(q) -\omega _R(p_3 -q) +i\epsilon }{\widetilde{E}_A -\omega _1(q) -\omega _R(p_3 +q) +i\epsilon } \right) , \end{aligned}$$
(47)

and since for the q of the singularity (q positive from now on)

$$\begin{aligned} \widetilde{E}_A -\omega _1(q) -\omega _R(p_3 -q) =0, \end{aligned}$$
(48)

then

$$\begin{aligned} \widetilde{E}_A -\omega _1(q) =\omega _R(p_3 -q), \end{aligned}$$
(49)

and we can write

$$\begin{aligned} t_t^{(0)}&= \frac{g_A \, g_R}{4 p_3 \, q}\, \ln \left( \frac{i \, \Gamma _R/2}{\omega _R(p_3 -q) -\omega _R(p_3 +q)}\right) \nonumber \\&\sim \frac{g_A \, g_R}{4 p_3 \, q}\, \ln \left( \frac{\Gamma _R}{\omega _R(p_3 -q) -\omega _R(p_3 +q)}\right) \end{aligned}$$
(50)

where we have substituted \(i\epsilon \) by \(i\frac{\Gamma _R}{2}\) and kept the singular part when \(\Gamma _R \rightarrow 0\). In the A decay width we shall have

$$\begin{aligned} \frac{d\Gamma _A^{(L)}}{dM_\mathrm{inv}(12)}&\propto \int _{-1}^{1} d\cos \theta \left| t_t^{(0)}\right| ^2\nonumber \\&\sim 2 \left( \frac{g_A \, g_R}{4 p_3 \, q}\right) ^2 \left| \ln \left( \frac{\Gamma _R}{\omega _R(p_3 -q) -\omega _R(p_3 +q)}\right) \right| ^2. \end{aligned}$$
(51)

On the other hand, we can look at the whole \(t_t\) amplitude, and the equivalent part to Eq. (51) going into the evaluation of the A width is, using Eq. (14),

$$\begin{aligned} \frac{d\Gamma _A^{(t)}}{dM_\mathrm{inv}(12)} \propto&\int _{-1}^{1} d\cos \theta \frac{g_A^2 \, g_R^2}{4 \,{\omega _R}^2(\vec {p}_3 -\vec {q}\,)}\nonumber \\&\quad \times \, \left| \frac{1}{\widetilde{E}_A -\omega _1(q) -\omega _R(\vec {p}_3 -\vec {q}\,) +i \frac{\Gamma _R}{2}} \right| ^2. \end{aligned}$$
(52)

Performing the same change of variable to the variable x of Eq. (33) we obtain

$$\begin{aligned} \frac{d\Gamma _A^{(t)}}{dM_\mathrm{inv}(12)}&\propto \frac{g_A^2 \, g_R^2}{4 p_3 \, q} \int _{\omega _R(p_3 -q)}^{\omega _R(p_3 +q)} dx \,\frac{1}{x}\,\nonumber \\&\quad \times \, \frac{1}{\left( \widetilde{E}_A -\omega _1(q) -x\right) ^2 +\left( \frac{\Gamma _R}{2}\right) ^2}. \end{aligned}$$
(53)

By making the change \(\widetilde{E}_A -\omega _1(q) -x = y\) and substituting \( \frac{1}{x}\) by its value in the singularity, \(\left[ \widetilde{E}_A -\omega _1(q)\right] ^{-1}\), we getFootnote 3

$$\begin{aligned} \frac{d\Gamma _A^{(t)}}{dM_\mathrm{inv}(12)}&\propto -\frac{1}{4 p_3 \, q}\, \frac{g_A^2 \, g_R^2}{\widetilde{E}_A -\omega _1(q)}\, \frac{2}{\Gamma _R}\nonumber \\&\quad \times \, \arctan \frac{2y}{\Gamma _R}\Bigg |_{\widetilde{E}_A -\omega _1(q)-\omega _R(p_3 -q)}^{\widetilde{E}_A -\omega _1(q)-\omega _R(p_3 +q)} \end{aligned}$$
(54)

where the lower limit in y vanishes. Hence we get

$$\begin{aligned}&\frac{d\Gamma _A^{(t)}}{dM_\mathrm{inv}(12)} \propto -\frac{1}{4 p_3 \, q}\, \frac{g_A^2 \, g_R^2}{\widetilde{E}_A -\omega _1(q)}\, \frac{2}{\Gamma _R}\nonumber \\&\quad \times \, \left\{ \arctan \frac{2\left( \omega _R(p_3 -q) -\omega _R(p_3 +q)\right) }{\Gamma _R} - \arctan \frac{0}{\Gamma _R} \right\} \end{aligned}$$
(55)

and since \(\omega _R(p_3 -q) < \omega _R(p_3 +q)\)

$$\begin{aligned} \lim _{\Gamma _R \rightarrow 0} \,\arctan \, \frac{2\left( \omega _R(p_3 -q) -\omega _R(p_3 +q)\right) }{\Gamma _R} = -\frac{\pi }{2}, \end{aligned}$$
(56)

and we get

$$\begin{aligned} \frac{d\Gamma _A^{(t)}}{dM_\mathrm{inv}(12)} \propto \frac{1}{4 p_3 \, q}\, \frac{g_A^2 \, g_R^2}{\widetilde{E}_A -\omega _1(q)}\, \frac{\pi }{\Gamma _R}. \end{aligned}$$
(57)

It is interesting to see that when \(\Gamma _R \rightarrow 0\), where the Schmid theorem holds, \(\Gamma _A\) from the tree level, Eq. (57), grows much faster than \(\Gamma _A\) from the triangle singularity from Eq. (51). This means, in a certain sense, that the Schmid theorem, even if true, becomes irrelevant, because in the limit where it holds, the contribution to the A width from the tree level is infinitely much larger than that from the triangle singularity.

Actually, \(\Gamma _A\) from Eqs. (51) and (57) do not diverge because \(g_R\) is related to the width. In fact, assuming \(2+3\) the only decay channel of R, for the S-wave coupling that we are considering we have

$$\begin{aligned} \Gamma _R = \frac{1}{8\pi }\, \frac{g_R^2}{M_R^2}\, \overline{q}, \end{aligned}$$
(58)

with \(\overline{q}\) the on shell momentum of particle 2 or 3 in \(R \rightarrow 2+3\) with R at rest. Then \(\Gamma _A\) from Eq. (57) goes to a constant, as it should be. If \(2+3\) is not the only decay channel then

$$\begin{aligned} \frac{g_R^2}{8\pi }\, \frac{1}{M_R^2}\, \overline{q} = \mathrm{BF}(2+3)\Gamma _R, \end{aligned}$$
(59)

where \(\mathrm{BF}(2+3)\) is the branching fraction of R to the \(2+3\) channel, and the conclusion is the same. In fact, in the limit \(\Gamma _R \rightarrow 0\), \(\Gamma _A\) calculated with the three body decay is exactly equal to \(\Gamma _A\) calculated from \(A \rightarrow R+1\) times the branching fraction \(\mathrm{BF}(2+3)\). This means that the contribution of the triangular singularity becomes negligibly small compared to the contribution of the whole tree level. However, if the width \(\Gamma _R\) is different from zero the ratio of contributions of the tree level to the triangle loop becomes finite, and many of the terms that we have been neglecting in the derivation of the Schmid theorem become relevant. Thus, one has to check numerically the contribution of the tree level and the triangle loop, summing them coherently, to see what comes out. This is particularly true when \(t_{12,12}\) sits on top of a resonance where the triangle singularity could be very important, or even dominant.

Yet, it is still interesting to note that in the realistic case the reaction studied still has a memory of Schmid theorem, in the sense that the coherent sum of amplitudes gives rise to a width, or cross section, that is even smaller than the incoherent sum of both contributions. One case where one can already check this is in the study of the \(\gamma \, p \rightarrow \pi ^0 \eta \, p\) reaction in Ref. [31]. The \(\gamma \, p\) couples to \(\Delta (1700)\) which decays to \(\eta \, \Delta (1232)\). The \(\Delta \) decays into \(\pi ^0 p\) and \(\eta \, p\) fuse to produce the \(N^*(1535)\) that subsequently decays into \(\eta \, p\). The contribution of this mechanism is sizable and has been observed experimentally [52]. In the study of Ref. [31] one compares the loop contribution with the tree level from \(\gamma \, p \rightarrow \Delta (1700) \rightarrow \eta \, \Delta (1232) \rightarrow \eta \pi ^0 p\) and they are of the same order of magnitude. A remarkable feature is that the coherent sum of tree level and loop does not change much the contribution of the tree level, even if the loop contribution is sizable, and is smaller than the incoherent sum of both processes (see Fig. 1 of Ref. [31]). Yet, even then, the \(N^*(1535)\) contribution to the \(\gamma p \rightarrow \pi ^0 \eta \, p\) gives a distinctive signature, both theoretically and experimentally. The message is clear: one must evaluate both the tree level and the loop contribution for each individual case to assert the relevance of the triangle singularity. Obviously in the case that the final channel is different from the internal one of the loop, there is no contribution of tree level and then the triangle singularity shows up clearly.

4 Considerations on the Dalitz plot

In Fig. 7 we show the Dalitz plot for a typical \(A \rightarrow 1+2+3\) process, where 1, 2, 3 are final states on shell. Recalling Eq. (8) that we reproduce again here

$$\begin{aligned} M_\mathrm{inv}^2(23) = M_A^2 +m_1^2 -2\widetilde{E}_A\widetilde{E}_1 +2\widetilde{p}_1\widetilde{p}_3\cos \theta , \end{aligned}$$
(60)

and that \(\widetilde{E}_A,\widetilde{E}_1,\widetilde{p}_1,\widetilde{p}_3\) all depend on \(M_\mathrm{inv}(12)\), by fixing \(M_\mathrm{inv}(12)\) Eq. (60) gives the limits of the Dalitz plot. For \(\cos \theta = -1\) we have the lower limit and for \(\cos \theta = 1\) we have the upper limit of the boundary of the Dalitz region. Let us cut the Dalitz boundary with a line of \(M_\mathrm{inv}(23) = M_R\). This line cuts the boundary in points A and D. In these points we have all final particles on shell and \(M_\mathrm{inv}(23) = M_R\). This is the situation of a triangle singularity provided that Eq. (27) is fulfilled (note that there are two solutions of q for \(\cos \theta =1\), but only one produces the triangle singularity, where in addition Eq. (27) is fulfilled). On the other hand, from point A to D, \(M_\mathrm{inv}(23) = M_R\) is allowed for some valid \(\cos \theta \) and we should expect a singularity (up to the factor \(g_R^2\)) of the tree level mechanism. Let us study this in detail.

In Eq. (57) we already saw the contribution of \(t_t\) to the A width evaluating \( \int _{-1}^{1}d\cos \theta \left| t_t\right| ^2\) at the point of the triangle singularity (point D in Fig. 7). Let us now evaluate it for an invariant mass \(M_\mathrm{inv}(12)\) between points A and D in the figure. Close to point A to the left we shall have now

$$\begin{aligned} \int _{-1}^{1}d\cos \theta \left| t_t\right| ^2 = -\frac{g_A^2 \, g_R^2}{4 p_3 \, q}\, \frac{1}{\widetilde{E}_A -\omega _1(q)}\, \frac{2}{\Gamma _R} \arctan \frac{2y}{\Gamma _R}\Bigg |_{y_2}^{y_1}, \end{aligned}$$
(61)

with \(y_1<0\) and \(y_2>0\), and hence

$$\begin{aligned} \lim _{\Gamma _R \rightarrow 0} \,\int _{-1}^{1}d\cos \theta \left| t_t\right| ^2&= -\frac{g_A^2 \, g_R^2}{4 p_3 \, q}\, \frac{1}{\widetilde{E}_A -\omega _1(q)}\, \frac{2}{\Gamma _R}\nonumber \\&\quad \times \, \left( -\frac{\pi }{2} -\frac{\pi }{2}\right) \end{aligned}$$
(62)

which is twice the result of Eq. (57). This value stabilizes as we move from A to D, and the interesting thing is that it goes like \((\Gamma _R)^{-1}\) (apart from the factor \(g_R^2\)). In addition we can evaluate \(\int _{-1}^{1}d\cos \theta \left| t_t\right| ^2\) for \(M_\mathrm{inv}(12)\) bigger than the one corresponding to point A. In this case R is never on shell and in the limit of small \(\Gamma _R\) we get zero contribution relative to the on shell one. Technically one would find it from Eq. (61) since now both \(y_1\) and \(y_2\) would be negative and the upper and lower limits of \(\arctan \frac{2y}{\Gamma _R}\) cancel.

5 Results

We are going to perform calculations with a particular case with the following configuration:

$$\begin{aligned} M_A&= 2154 \, \mathrm{MeV}\nonumber \\ M_R&= 1600 \, \mathrm{MeV}, \quad \Gamma _R = 30 \, \mathrm{MeV}\nonumber \\ M_1&= 500 \, \mathrm{MeV}\nonumber \\ M_2&= 200 \, \mathrm{MeV}\nonumber \\ M_3&= 900 \, \mathrm{MeV}. \end{aligned}$$
(63)

In addition we shall take an amplitude \(1+2 \rightarrow 1+2\) parameterized in terms of a Breit-Wigner form

$$\begin{aligned} t_{12,12} = \frac{g^2}{M_\mathrm{inv}^2(12) -M_\mathrm{BW}^2 +i \, \Gamma _{BW}(M_\mathrm{inv}(12))M_\mathrm{inv}(12)}, \end{aligned}$$
(64)

with \(M_\mathrm{BW} = 800\ \hbox {MeV}\), \(\Gamma _{BW} = 20\ \hbox {MeV}\). We shall use Eq. (20) and choose \(g^2\) such that the width is given by Eq. (58). In this case we have purely elastic scattering and \(g=1338.7\ \hbox {MeV}\). We will also consider the case where we take the same value of g and a width double the elastic one to account for inelasticities, to test what happens in the case of inelastic channels.

We will use Eqs. (14) and (18) and integrate Eq. (12) over \(M_\mathrm{inv}(23)\) to obtain \(d\Gamma _A/d M_\mathrm{inv}(12)\). Note that according to Eq. (8) the integral over \(\cos \theta \) that we have done is simply \(2 M_\mathrm{inv}(23) d M_\mathrm{inv}(23) / 2 \widetilde{p}_1 \widetilde{p}_3\). The limits of integration are obtained from Eq. (8) for \(\cos \theta = \pm 1\), and explicit formulas can be obtained from the PDG [48]. In Eq. (18) we have used a cutoff in the q integration of \(600\ \hbox {MeV}\), a common value in many of these problems.

The choice of variables in Eqs. (63) and (64) is done such that Eq. (27) is satisfied and we have a triangle singularity for this configuration.

In Fig. 7 we show the Dalitz plot for the reaction \(A \rightarrow 1+2+3\). We can indeed see that the triangle singularity point corresponds to point D of Fig. 7.

Fig. 7
figure 7

Dalitz plot for \(A \rightarrow 1+2+3\) with the parameters of Eqs. (63) and (64). Point D corresponds to the triangle singularity

In the first case we evaluate \(d\Gamma _A/d M_\mathrm{inv}(12)\) for \(M_A =2200\ \hbox {MeV}\), about \(50\ \hbox {MeV}\) above the mass that leads to a triangle singularity at \(M_\mathrm{inv}(12) = 800\ \hbox {MeV}\). With this value of \(M_A\), the triangle singularity appears at \(M_\mathrm{inv}(12) = 769\ \hbox {MeV}\), about \(30\ \hbox {MeV}\) below the Breit-Wigner mass. We can expect that the loop function will give a small contribution, since \(t_{12,12}\) at this invariant mass is significantly reduced compared to its peak. Yet, this serves us to investigate the points discussed in the former section.

In Fig. 8 we show \(d\Gamma _A/d M_\mathrm{inv}(12)/g_A^2 \, g_R^2\) as a function of \(M_\mathrm{inv}(12)\). We show the results for the triangle diagram alone, the tree level alone, and the coherent sum for \(\Gamma _R = 30\ \hbox {MeV}\).

Fig. 8
figure 8

\( \frac{d\Gamma _A}{d M_\mathrm{inv}(12)}\,\frac{1}{g_A^2 \, g_R^2}\) as a function of \(M_\mathrm{inv}(12)\) with \(M_A = 2200\ \hbox {MeV}\) and \(\Gamma _R = 30\ \hbox {MeV}\)

As we have discussed previously, we have proved the Schmid theorem in the limit of \(\Gamma _R \rightarrow 0\). Figure 8 gives us the answer of what happens when we look at a realistic case with \(\Gamma _R\) of the order of tens of MeV. As we can see, the triangle loop gives a sizable contribution of the order of the tree level, and the coherent sum of the triangle diagram and the tree level diagram gives rise to a very distinct structure, as a consequence of the resonance in the 1, 2 channel enhanced by the triangle diagram. This already tell us that in a realistic calculation we should not rely on the Schmid theorem to neglect the triangle diagram with elastic rescattering of the internal particles of the loop.

In Fig. 9 we show the same results but calculated with \(\Gamma _R = 0.5\ \hbox {MeV}\).

Fig. 9
figure 9

\( \frac{d\Gamma _A}{d M_\mathrm{inv}(12)}\,\frac{1}{g_A^2 \, g_R^2}\) as a function of \(M_\mathrm{inv}(12)\) with \(M_A = 2200\ \hbox {MeV}\) and \(\Gamma _R = 0.5\ \hbox {MeV}\). The dashed and solid lines are indistinguishable in the figure

As we can see, the triangle singularity gives a small contribution compared to the tree level, and the coherent sum of the two does not change the contribution of the tree level, as expected from the Schmid theorem. In Fig. 10 we show the same results but calculated with \(\Gamma _R = 0.1\ \hbox {MeV}\). Comparing these results with those of Fig. 9, we can see that as \(\Gamma _R\) is made smaller the tree level contribution grows more or less like \(1/\Gamma _R\), as expected from Eq. (57), while the triangle contribution grows much less.

Fig. 10
figure 10

\( \frac{d\Gamma _A}{d M_\mathrm{inv}(12)}\,\frac{1}{g_A^2 \, g_R^2}\) as a function of \(M_\mathrm{inv}(12)\) with \(M_A = 2200\ \hbox {MeV}\) and \(\Gamma _R = 0.1\ \hbox {MeV}\). The dashed and solid lines are indistinguishable in the figure

In Fig. 11 we show again the results for the same \(M_A\) mass and \(\Gamma _R = 0.1\ \hbox {MeV}\), but this time we take in Eq. (64) \(\Gamma _{BW} \rightarrow 2\Gamma _{BW}\) to account for the inelasticities.

Fig. 11
figure 11

\( \frac{d\Gamma _A}{d M_\mathrm{inv}(12)}\,\frac{1}{g_A^2 \, g_R^2}\) as a function of \(M_\mathrm{inv}(12)\) with \(M_A = 2200\ \hbox {MeV}\) and \(\Gamma _R = 0.1\ \hbox {MeV}\). Here \(\Gamma _{BW} \rightarrow 2\Gamma _{BW}\) to account for the inelasticities. The dashed and solid lines are indistinguishable in the figure

The contribution of the triangle loop is reduced with respect to the one in the elastic case of Fig. 10. Curiously, the relative strength of the singularity (narrow peak in the dotted line) with respect to the resonance peak increases now, as a reminder that according to Eq. (46) the Schmid theorem does not hold. Yet, the main message from Figs. 9, 10 and 11 is that in the limit of \(\Gamma _R \rightarrow 0\), where the Schmid theorem holds, the relative strength of the triangle diagram versus the tree level becomes negligible.

Next we perform the calculations for \(M_A = 2154\ \hbox {MeV}\), first for \(\Gamma _R=0.1\ \hbox {MeV}\), and show the results in Fig. 12.

Fig. 12
figure 12

\( \frac{d\Gamma _A}{d M_\mathrm{inv}(12)}\,\frac{1}{g_A^2 \, g_R^2}\) as a function of \(M_\mathrm{inv}(12)\) with \(M_A = 2154\ \hbox {MeV}\) and \(\Gamma _R = 0.1\ \hbox {MeV}\). The dashed and solid lines are indistinguishable in the figure

The novelty in this case is that, since the triangle singularity occurs for \(M_\mathrm{inv}(12) =800\ \hbox {MeV}\), equal to \(M_\mathrm{BW}\), now the contribution of the triangle mechanism is much bigger than in the former cases. Yet, relative to the tree level its strength is very small and in the coherent sum one does not appreciate its contribution, as was the case of Figs. 9 and 10, in agreement with the Schmid theorem. Actually this is a good case to show the effects of the Schmid theorem, since the strength of the peak is about \(10^{-2}\) the one of the tree level. This implies a factor \(10^{-1}\) in the amplitude, and in an ordinary coherent sum of these two amplitudes one might expect a contribution of about 20% in the differential width, which is not the case in Fig. 12. Yet we should stress once more that the triangle mechanism becomes negligible on its own, independently of the Schmid theorem, when \(\Gamma _R \rightarrow 0\).

In Fig. 13 we show the same results now for \(\Gamma _R =30\ \hbox {MeV}\). We can see now that the effect of the triangle singularity shows in \( \frac{d\Gamma _A}{d M_\mathrm{inv}(12)}\). However, it is interesting to see that the coherent sum of the tree level and the triangle singularity is smaller than their incoherent sum, indicating that, although one is in a region where the Schmid theorem does not strictly hold, the process still has some memory of the the absorption of the triangle mechanism by the tree level amplitude that occurs in the limit of small \(\Gamma _R\).

We should also note that if we make \(\Gamma _R\) bigger the relative strength of the loop contribution to the tree level grows and can become dominant at the invariant mass of the triangle singularity.

6 Conclusions

We have done a new derivation of the Schmid theorem and have studied the results as a function of \(\Gamma _R\), the width of the intermediate state in the triangle loop that decays into an external particle and an internal one. The Schmid theorem holds strictly in the limit when \(\Gamma _R \rightarrow 0\). We show this again and illustrate it with a numerical example.

The first thing that we find is that when \(\Gamma _R \rightarrow 0\) the relative weight of the triangle singularity versus the tree level contribution goes to zero. This means that, in a strict sense, the Schmid theorem would be irrelevant because where it holds and shows that the singularity changes only the phase of the S-wave part of the tree level amplitude, \(t_t^{(0)}\), the strength of the triangle diagram or of \(t_t^{(0)}\) is very small compared with the whole contribution of the full tree level amplitude.

We conducted some tests to see what happens when we have \(\Gamma _R\) finite and also when the scattering amplitude of the two particles that interact in the loop sit on top of a resonance.

Fig. 13
figure 13

\( \frac{d\Gamma _A}{d M_\mathrm{inv}(12)}\,\frac{1}{g_A^2 \, g_R^2}\) as a function of \(M_\mathrm{inv}(12)\) with \(M_A = 2154\ \hbox {MeV}\) and \(\Gamma _R = 30\ \hbox {MeV}\)

In general lines we see that for finite \(\Gamma _R\) widths the Schmid theorem does not strictly hold but the \(A \rightarrow 1+2+3\) process still has some memory of the theorem in the sense that the coherent sum of tree level and triangle singularity gives rise to a differential width where the interference is much smaller than usual, with final results even smaller than the incoherent sum of the two mechanisms.

We also saw that in the case of a \(1+2 \rightarrow 1+2\) scattering amplitude with inelasticities the Schmid theorem does not hold and we could quantify the contribution of the triangle singularity, both analytically and numerically in the example we discussed.

The biggest contribution of the triangle singularity appears when the \(1+2 \rightarrow 1+2\) scattering amplitude sits on top of a resonance. In this case, and for finite \(\Gamma _R\), the contribution of the triangle singularity shows up clearly and can be even dominant over the tree level in some cases.

The message in general is that for each particular case one has to calculate both the tree level and the triangle mechanism and sum them coherently to see what comes out. Invoking the Schmid theorem to rule out the triangle mechanism in the case that the rescattering of particles 1, 2 goes to the same channel should not be done.