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Near to short wave infrared light generation through AlGaAs-on-insulator nanoantennas

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Abstract

AlGaAs-on-insulator (AlGaAs-OI) has recently emerged as a promising platform for nonlinear optics at the nanoscale. Among the most remarkable outcomes, second-harmonic generation (SHG) in the visible/near infrared spectral region has been demonstrated in AlGaAs-OI nanoantennas (NAs). In order to extend the nonlinear frequency generation towards the short wave infrared window, in this work we propose and demonstrate via numerical simulations difference frequency generation (DFG) in AlGaAs-OI NAs. The NA geometry is finely adjusted in order to obtain simultaneous optical resonances at the pump, signal and idler wavelengths, which results in an efficient DFG with conversion efficiencies up to 0.01%. Our investigation includes the study of the robustness against random variations of the NA geometry that may occur at fabrication stage. Overall, these outcomes identify what we believe to be a new potential and yet unexplored application of AlGaAs-OI NAs as compact devices for the generation and control of the radiation pattern in the near to short infrared spectral region.

Published by Optica Publishing Group under the terms of the Creative Commons Attribution 4.0 License. Further distribution of this work must maintain attribution to the author(s) and the published article's title, journal citation, and DOI.

1. Introduction

In the last few years AlGaAs-on-insulator (AlGaAs-OI) has emerged as a novel promising platform for nonlinear optics [17]. Differently from standard AlGaAs devices grown on their native GaAs substrate, AlGaAs-OI benefits from a low-index cladding that allows for strong mode confinement, which in turn enhances the optical nonlinear response of AlGaAs [811]. Among the AlGaAs-OI devices of interest for nonlinear optics, we can distinguish between long (few millimetres/centimetres) waveguides, fabricated via wafer bonding and electron beam lithography [12], and compact (sub-micron to few microns long) nanoantennas (NAs), typically fabricated via molecular beam epitaxy [13]. While phase matching is the leading mechanism to achieve relevant nonlinear conversion in waveguides, in NAs the nonlinear processes are boosted by cavity resonances at the involved wavelengths [8].

Recently, AlGaAs-OI NAs have been proposed to mold and tune the radiation pattern of second-harmonic generation (SHG) at the nanoscale in the visible/near-infrared region of the electromagnetic spectrum ($\sim 800$ nm) [1418]. Indeed, in contrast with the plasmonic counterpart, this all-dielectric solution combines large nonlinearities and low optical losses.

An exciting but yet unexplored evolution of these outcomes is light generation in the near/short wave infrared (wavelengths beyond 1400 nm) via difference frequency generation (DFG). This spectral region is important for applications ranging from medicine and biology to telecommunications [19]. While substantial near/mid-infrared generation through DFG has been reported in standard few centimeters long LiNbO$_3$ [20] and AlGaAs waveguides [21,22], to the best of our knowledge there has been little to no attempt to demonstrate DFG in compact sub-micrometer or few-micrometers long all-dielectric devices. Inspired by the recent achievements in SHG and spontaneous parametric down-conversion (SPDC) [23], in this manuscript we report on the design of compact AlGaAs NAs for near/short wave infrared generation through DFG. The envisaged setup is sketched in Fig. 1, where two intense beams, conventionally named pump and signal, illuminate the NA and generate a new wavelength, named idler, through DFG. Differently from the case of SHG, which requires resonances at the fundamental and the second-harmonic frequencies, the design of NAs for DFG is further complicated by the requirement of resonances at all the three frequencies into play [24]. Section 2 is dedicated to the design of NAs that are simultaneously resonant at pump, signal and idler. In Section 3, the nonlinear system of equations coupling pump, signal and idler is solved numerically taking into account the anisotropic second-order nonlinear response of AlGaAs, and we identify the most suitable configurations to maximise idler generation. Finally in Section 4, we discuss the robustness of our method against fabrication imperfections by showing how the variation of the geometrical parameters may affect the DFG conversion efficiency (CE).

 figure: Fig. 1.

Fig. 1. Sketch of the setup: the incident pump (blue) and signal (green) plane waves propagate along the $y$ direction and are $x-$polarised. The idler radiation (red) is generated via difference frequency generation and is z-polarized. The Cartesian coordinate system in the figure shows the orientation of the crystal axes of AlGaAs.

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2. Resonance analysis

We consider a cylindrical AlGaAs NA with its axis oriented along the longitudinal direction z and fully embedded in an insulator. Among the possible choices for the cladding, silica [25] and hydrogen silsesquioxane (HSQ) [10,12] stand out for their low index. For the sake of exemplification, here we focus on silica, but the present results might be readily generalized to HSQ cladding, the latter yielding a similar refractive index. We assume that the incident beams size is substantially larger than the NA dimensions, so that the beams can be modelled as plane waves. Pump and signal beams with angular frequencies $\omega _p$ and $\omega _s$ illuminate the NA. We focus on the case where the illumination occurs laterally, i.e. the wave-vectors of the incident plane waves are parallel to the y-direction and the electric fields are polarized along x, as displayed in Fig. 1. In this way, by exploiting the length of the NA we maximize the illuminated surface and the total energy that can be converted by DFG. Moreover, we assume that the antenna length $L$ is substantially larger than its transverse dimension $d$ ($L/d\gg 1$) and the wavelengths into play ($L/\lambda \gg 1$), therefore a few-microns long at least. Note that, for notation simplicity, despite this assumption here we still use the term “nanoantenna”. Similarly to slab waveguides, which are characterised by ratios $L/d\gg 1$, $L/\lambda \gg 1$ and are therefore approximated as infinite in the length direction, so in the case under investigation we can approximate the antenna as a 2D object (in the x-y plane) with indefinite length along the z-direction, which on its turn reduces the numerical load and simplifies the interpretation of the results. In order to further simplify the complex numerical design, we limit our investigation to antennas with circular cross-sections and a sub-micron radius.

The interaction between the scattered pump and signal fields inside the NA generates the idler (angular frequency $\omega _i$) via DFG. The crystalline axes of the AlGaAs are aligned with the reference frame reported in Fig. 1. AlGaAs has a nonlinear second-order susceptibility tensor $\chi ^{(2)}_{ijk}=100$ pm/V if $i\neq j \neq k$, and $\chi ^{(2)}_{ijk}=0$ otherwise [8].

We look for those NA cross-sections that exhibit three resonances at the pump, signal and idler frequencies and that satisfy the DFG energy conservation relation:

$$\omega_i=\omega_p-\omega_s.$$

Note that in the following we use interchangeably the frequencies $\omega _{p,s,i}$ and the corresponding wavelengths $\lambda _{p,s,i}=2\pi c/\omega _{p,s,i}$ ($c$ being the speed of light in free space).

To find the suitable resonances, we use finite element simulations (COMSOL Multiphysics) [2631] to calculate the electromagnetic energy density per unit length ($E_d$) stored in the NA as a function of wavelength, when the NA is excited by a x-polarised plane wave (Fig. 2(a)). The peaks of the stored energy density identify the available pump and signal resonances.

 figure: Fig. 2.

Fig. 2. Electromagnetic energy density ($E_d$) stored within the circular NA ($r=740$ nm) when excited by a x-polarised (panel a) or z-polarised (panel b) plane wave. The insets display the norm of the electric field at the pump ($\lambda =$ 801 nm, blue arrow), signal ($\lambda =1446$ nm, green arrow) and idler ($\lambda = 1796$ nm, red arrow) resonances.

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According to the AlGaAs nonlinear tensor ($\chi _{ijk}^{(2)}\neq 0$ for $i\neq j\neq k$), a non-zero z-component of the scattered signal or pump electric field would be required in order to have a non-zero x or y- component of the idler electric field. However, in the 2D geometry under study with lateral illumination, the z-component of the signal and pump is null. Therefore, the generated idler electric field has null x and y component, namely, it is oriented parallel to the z-axis. In Fig. 2(b) we report the energy density corresponding to an excitation with a z-polarised plane wave, from which we identify the idler resonances that are potentially available for the DFG process. The refractive indices of the Al$_{\xi }$Ga$_{1-\xi }$ As core and the silica cladding are taken from [32] and [33], respectively, $\xi \approx 0.2$ being the standard value used in SHG processes to minimize the optical losses when the pump is at telecom wavelengths ($\sim$ 1550 nm).

Here, we report a NA with circular cross-section and with three resonances at the frequencies satisfying the condition in Eq. (1). Indeed, when the NA radius is $r=740$ nm, pump, signal and idler resonances are at wavelengths of 801 nm, 1446 nm and 1796 nm, respectively, as highlighted by the arrows in Fig. 2. As it can be seen from the electric field profile reported in the insets in Fig. 2, the three resonances correspond to whispering gallery modes (WGMs) and thus present higher quality factors with respect to usual Mie-type resonances in dielectric NAs [8,13]. Indeed, the quality factor $Q_j=\omega _j/\Delta \omega _j$ (with $j={p,s,i}$ and $\Delta \omega _j$ being the resonance line-width), is 2000, 300 and 1800 at the pump, signal and idler frequencies, respectively.

3. DFG conversion efficiency

In this section, we discuss a fully-coupled numerical model implemented with finite element method to simulate the DFG process and then to compute the idler CE in the above-mentioned circular NA. An extensive description of the model is provided in Ref. [22]. The Maxwell’s equations describing the evolution of the electric field $\mathbf {E}$ at the pump, signal and idler frequencies read as:

$$\nabla \times\left( \nabla \times \mathbf{E}\left(\omega_{n}\right)\right)-k_{0}^{2}\left(\omega_{n}\right)\varepsilon_{r} \mathbf{E}\left(\omega_{n}\right)=\mu_{0} \omega_{n}^{2} \mathbf{P}^{(2)}\left(\omega_{n}\right),$$
with $n=p,s,i$. The 3 frequencies are coupled through the quadratic nonlinear polarization vector $\mathbf {P}^{(2)}$, which for AlGaAs reads as:
$$\left\{ \begin{array}{l} P^{(2)}_a(\omega_p)=\varepsilon_0\chi^{(2)}\left[E_b(\omega_s)E_c(\omega_i)+E_c(\omega_s)E_b(\omega_i)\right]\\ P^{(2)}_a(\omega_s)=\varepsilon_0\chi^{(2)}\left[E_b(\omega_p)E_c^*(\omega_i)+E_c(\omega_p)E_b^*(\omega_i)\right]\\ P^{(2)}_a(\omega_i)=\varepsilon_0\chi^{(2)}\left[E_b(\omega_p)E_c^*(\omega_s)+E_c(\omega_p)E_b^*(\omega_s)\right],\\ \end{array} \right.$$
where $a,b,c\in \{x,y,z\}$, with $a\neq b\neq c$. The incident field for pump and signal is represented by x-polarised plane waves with intensities $I_p$ and $I_s$, respectively. On the other hand, the incident idler field is null; idler is indeed generated as a result of the nonlinear coupling among pump and signal inside the NA.

In analogy with the case of SHG reported in [8], the CE is defined as the ratio of the generated idler power to the total (signal + pump) incident power. In the system under analysis the NA exhibits translation symmetry along the z-direction, therefore the efficiency reduces to the following formula:

$$\eta=\frac{\oint_\gamma \mathbf{S}(\omega_i)\cdot \mathbf{n} d\gamma}{2r(I_s+I_p)}.$$
where $\mathbf {S}(\omega _i)$ is the Poynting vector at the idler frequency, $\gamma$ is a closed line containing the NA circular cross section and $\mathbf {n}$ is the normal unit vector pointing outside the adopted closed line.

In Fig. 3(a) we report $\eta$ as function of the pump ($\lambda _p$) and signal ($\lambda _s$) wavelengths when pump and signal intensities are $I_s=I_p=$ 1 GW/cm$^2$. It is worth noting that this or even higher values (1-10 GW/cm$^2$) of intensity have been employed for efficient second-harmonic generation in NAs [13,16,34,35]. Three bright striped regions stand out where the DFG conversion is remarkable. The vertical and horizontal stripes are centered around the pump and signal resonances. This is not surprising, as the DFG is boosted by the enhanced electric field of both pump and signal when they are resonant. Similarly, the diagonal stripe turns out to be the region where the idler is resonant. Indeed, in Fig. 3(b) we plot in yellow the region of the plane $(\lambda _p,\lambda _s)$ where the idler wavelength $\lambda _i=(\lambda _p^{-1}-\lambda _s^{-1})^{-1}$ is in the range $1796\pm 2$ nm, that is to say, close to the idler resonance. We observe that the yellow region in Fig. 3(b) matches well the bright diagonal stripe of Fig. 3(a). In conclusion, Fig. 3(a) shows that the DFG conversion is enhanced when any of the pump, signal or idler wavelength is resonant. On the other hand, the peak of conversion is obtained when pump, signal and idler are simultaneously resonant, namely, at the intersection between the 3 bright striped regions. For the considered NA, this occurs for $\lambda _p=801$ nm and $\lambda _s=1446$ nm (corresponding to $\lambda _i=1796$ nm). Consequently, the shape of the generated idler field, reported in Fig. 3(c), matches well with the field in the inset of Fig. 2(b), thus proving that the DFG process we propose relies on three resonant modes of the NAs. The achieved maximum CE $\eta _{max}\sim 2.5\times 10^{-4}$ is in line with the CE previously obtained for SHG processes when similar values of pump intensity are employed [13].

 figure: Fig. 3.

Fig. 3. a) DFG CE $\eta$ (the logarithm is used to highlight the contrast) as function of the signal and pump wavelengths. The pump and signal incident intensity is $I_p=I_s=1$ GW/cm$^2$. The blue and green arrows on the top and on the left side indicate the resonant wavelengths for pump (801 nm) and signal (1446 nm), respectively. b) Plane as in panel a) displaying the regions where the corresponding idler wavelength $\lambda _i=(\lambda _p^{-1}-\lambda _s^{-1})^{-1}$ is close to its resonance (i.e. in the range $1796\pm 2$ nm), highlighted with a yellow stripe, or far from the resonance (blue). c) Generated electric field (norm) of the idler when $\lambda _p=801$ nm and $\lambda _s=1446$ nm. A circular NA with radius $r=740$ nm is considered here.

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4. Conversion efficiency robustness upon variation of the geometrical parameters

In this section, we discuss how the variation of the geometrical parameters of the NA affects the CE. In particular, due to experimental tolerances, it is quite challenging to fabricate a perfectly circular NA, but rather an elliptical NA is more likely. For this reason, in this section we consider the CE generated by an elliptical NA, whose semi-axes are $r_x$ and $r_y$ (as schematized in the inset of Fig. 4). In Fig. 4, we report the CE as function of $r_x$ and $r_y$. The incident pump and signal are polarized along $x$, their wave vector is parallel to $y$, their intensity is 1 GW/cm$^2$ and their wavelengths are 801 nm and 1446 nm, respectively.

 figure: Fig. 4.

Fig. 4. DFG CE $\eta$ (the logarithm is used to highlight the contrast) as function of the two ellipse semi-axes $r_x$ and $r_y$. The wavelength of the incident pump and signal is fixed to 801 nm and 1446 nm, respectively. The intensity of both beams is set to 1 GW/cm$^2$. Inset: Sketch of the elliptic nanoantenna and the illuminating electric field (E$_{inc}$).

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When $r_x=r_y=740$ nm we recover the circular NA described in the previous sections and the CE is high. Moreover, we note that the CE can be even further enhanced up to $3.9\times 10^{-4}$ for $r_x=750$ nm and $r_y=730$ nm. On the other hand, this remarkable CE comes at the expenses of a strong sensitivity to small variations of the geometric parameters. For example, we observe that the CE drops by 2 orders of magnitude if $r_x=755$ nm and and $r_y=730$, reaching the value of $\eta =7\times 10^{-6}$. For this reason, these very efficient configurations are quite sensitive to fabrication imperfections and a small variation on the geometry may considerably reduce the CE.

A possible way to overcome this problem is to move towards the top left corner of Fig. 4, i.e. semi-axes $r_x\sim 720$ nm and $r_y\sim 760$ nm. Despite in this region the CE is lower ($\eta <10^{-5}$), however it is weakly affected by semi-axes variations as large as 10 nm. The map of the CE as function of the pump and signal wavelengths for the case $r_x=720$ nm and $r_y=760$ nm is reported in Fig. 5. As for the case illustrated in Fig. 3(a), the bright diagonal stripe corresponds to a resonant idler. However, differently from Fig. 3(a), pump and signal resonances have a minor impact on the CE. Indeed, the CE computed when the idler is resonant but the pump and signal are not is of the same order of magnitude (only 2 times smaller) than the case where pump, signal and idler are simultaneously resonant (blue and green arrows in Fig. 5). The latter trend may be explained by looking at the electromagnetic energy density ($E_d$) stored at pump, signal and idler wavelengths, calculated with linear simulations (Fig. 6). While for pump and signal $E_d$ varies by a factor of 2 outside the respective resonances (as depicted in Fig. 6(a)), on the contrary the variation is substantial in the case of the idler (e.g. about a factor 7 between wavelengths at 1796 nm and at 1750 nm, see Fig. 6(b)). On the other hand, in the efficient case in Fig. 3(a) all the three resonances showed an energy density changing more than one order of magnitude passing from the maximum to the minimum. Thus, the efficient case is also more sensitive to small variations of the geometry than the design reported in Fig. 5.

 figure: Fig. 5.

Fig. 5. DFG CE $\eta$ as a function of the signal and pump wavelengths, for an elliptical NA with $r_x=720$ nm and $r_y=760$ nm. The pump and signal incident intensity is $I_p=I_s=1$ GW/cm$^2$. The blue and green arrows on the top and on the left side indicate the resonant wavelengths for pump (801 nm) and signal (1446 nm), respectively.

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 figure: Fig. 6.

Fig. 6. Electromagnetic energy density ($E_d$) stored within the elliptical NA ($r_x=720$ nm and $r_y=760$ nm) when the NA is excited by a x-polarised (panel a) or z-polarised (panel b) plane wave. The blue, green and red arrows identify the pump ($\lambda = 801$ nm), signal ($\lambda = 1446$ nm) and idler ($\lambda = 1796$ nm) resonances.

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5. Conclusion

AlGaAs-OI has recently emerged as a promising platform for nonlinear nano-optics. In the last few years, several works have addressed second-harmonic generation, sum-frequency generation and spontaneous parametric down conversion in the visible/near-infrared spectrum by means of AlGaAs-OI NAs. In this paper we extended the operation in the near/short wave infrared spectral region via DFG.

We identified a NA with circular cross-section exhibiting simultaneous resonances at three distinct wavelengths that satisfy the DFG energy conservation relation. The corresponding CE is comparable with the CE obtained via SHG processes [13].

We investigated how the variation of the geometrical parameters may affect the CE. The latter seems to be substantially sensitive to variations of a few nanometers in the case of multi-resonant NAs, which may pose a challenge at fabrication stage. However, we have identified a further configuration based on an elliptical NA where the idler resonance is dominant, which is characterized by a lower CE but is remarkably more robust against geometrical perturbations.

We have focused our investigation on the special case where the NA length is substantially larger than the diameter and the wavelengths into play ($L/d\gg 1$, $L/\lambda \gg 1$), which allows employing a 2D representation that drastically reduces the computational cost. AlGaAs nanowires represent an example where the above-mentioned conditions ($L/d\gg 1$, $L/\lambda \gg 1$) apply [36,37]. In addition, our analysis could be easily adapted to NAs with arbitrary shape, which paves the way for further scenarios. For example, AlGaAs NAs with rectangular base and arbitrary ratio $L/d_{1,2}\gg 1$ ($d_{1,2}$ being the transverse dimensions) could be fabricated on-chip via standard techniques used for integrated waveguides [10,11,25]. In this case, lateral illumination and DFG characterisation could be achieved either via free-space coupling [38] or via a dedicated coupling system based on integrated tapers and/or gratings.

Note that a full 3D numerical investigation would follow the same logic as in the 2D case discussed in this work. For example, in the case of NAs with circular base, the search for the resonant wavelengths would be done as a function of both the NA radius and length, and for illumination with arbitrary tilt angle. However, the main challenge in the 3D case is represented by the computational cost, which makes the analysis prohibitively time consuming for the computational resources at our disposal.

In conclusion, these outcomes identify a new potential application of AlGaAs-OI NAs as compact devices for the generation and control of light in the near to short wave infrared spectral region. We expect that resorting to different or more complex geometries (e.g., NA with rectangular cross-section, coupled NAs, arrays or metasurfaces) one may further increase the efficiency and spectral tunability of the generated radiation, even reaching DFG generation in the mid-infrared region. Our results illustrate potential for the design of quantum photonic structures via DFG-SPDC reciprocity [39,23] and for the development of new nanoscale sources of light at near-short infrared frequencies.

Funding

Horizon 2020 Framework Programme (899673, 802682); Ministero dell’Istruzione, dell’Università e della Ricerca (2020EY2LJT_002); Ministero dell’Istruzione, dell’Università e della Ricerca (2017MP7F8F); Russian Science Foundation (22-12-00204); Engineering and Physical Sciences Research Council (EP/T019441/1).

Acknowledgments

M. Gandolfi and A. Tognazzi acknowledge the European Union for the financial support through FESR o FSE, PON Ricerca e Innovazione 2014-2020 - DM 1062/2021. A. Tognazzi acknowledges the financial support from the University of Palermo through Fondo Finalizzato alla Ricerca di Ateneo 2023 (FFR2023).

Disclosures

The authors declare no conflicts of interest.

Data availability

Data underlying the results may be obtained from the authors upon reasonable request.

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Data availability

Data underlying the results may be obtained from the authors upon reasonable request.

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Figures (6)

Fig. 1.
Fig. 1. Sketch of the setup: the incident pump (blue) and signal (green) plane waves propagate along the $y$ direction and are $x-$ polarised. The idler radiation (red) is generated via difference frequency generation and is z-polarized. The Cartesian coordinate system in the figure shows the orientation of the crystal axes of AlGaAs.
Fig. 2.
Fig. 2. Electromagnetic energy density ( $E_d$ ) stored within the circular NA ( $r=740$ nm) when excited by a x-polarised (panel a) or z-polarised (panel b) plane wave. The insets display the norm of the electric field at the pump ( $\lambda =$ 801 nm, blue arrow), signal ( $\lambda =1446$ nm, green arrow) and idler ( $\lambda = 1796$ nm, red arrow) resonances.
Fig. 3.
Fig. 3. a) DFG CE $\eta$ (the logarithm is used to highlight the contrast) as function of the signal and pump wavelengths. The pump and signal incident intensity is $I_p=I_s=1$ GW/cm $^2$ . The blue and green arrows on the top and on the left side indicate the resonant wavelengths for pump (801 nm) and signal (1446 nm), respectively. b) Plane as in panel a) displaying the regions where the corresponding idler wavelength $\lambda _i=(\lambda _p^{-1}-\lambda _s^{-1})^{-1}$ is close to its resonance (i.e. in the range $1796\pm 2$ nm), highlighted with a yellow stripe, or far from the resonance (blue). c) Generated electric field (norm) of the idler when $\lambda _p=801$ nm and $\lambda _s=1446$ nm. A circular NA with radius $r=740$ nm is considered here.
Fig. 4.
Fig. 4. DFG CE $\eta$ (the logarithm is used to highlight the contrast) as function of the two ellipse semi-axes $r_x$ and $r_y$ . The wavelength of the incident pump and signal is fixed to 801 nm and 1446 nm, respectively. The intensity of both beams is set to 1 GW/cm $^2$ . Inset: Sketch of the elliptic nanoantenna and the illuminating electric field (E $_{inc}$ ).
Fig. 5.
Fig. 5. DFG CE $\eta$ as a function of the signal and pump wavelengths, for an elliptical NA with $r_x=720$ nm and $r_y=760$ nm. The pump and signal incident intensity is $I_p=I_s=1$ GW/cm $^2$ . The blue and green arrows on the top and on the left side indicate the resonant wavelengths for pump (801 nm) and signal (1446 nm), respectively.
Fig. 6.
Fig. 6. Electromagnetic energy density ( $E_d$ ) stored within the elliptical NA ( $r_x=720$ nm and $r_y=760$ nm) when the NA is excited by a x-polarised (panel a) or z-polarised (panel b) plane wave. The blue, green and red arrows identify the pump ( $\lambda = 801$ nm), signal ( $\lambda = 1446$ nm) and idler ( $\lambda = 1796$ nm) resonances.

Equations (4)

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ω i = ω p ω s .
× ( × E ( ω n ) ) k 0 2 ( ω n ) ε r E ( ω n ) = μ 0 ω n 2 P ( 2 ) ( ω n ) ,
{ P a ( 2 ) ( ω p ) = ε 0 χ ( 2 ) [ E b ( ω s ) E c ( ω i ) + E c ( ω s ) E b ( ω i ) ] P a ( 2 ) ( ω s ) = ε 0 χ ( 2 ) [ E b ( ω p ) E c ( ω i ) + E c ( ω p ) E b ( ω i ) ] P a ( 2 ) ( ω i ) = ε 0 χ ( 2 ) [ E b ( ω p ) E c ( ω s ) + E c ( ω p ) E b ( ω s ) ] ,
η = γ S ( ω i ) n d γ 2 r ( I s + I p ) .
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