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Polarization spectroscopy of dressed four-wave mixing in a three-level atomic system

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Abstract

Polarization properties of pure four-wave mixing (FWM) and dressed-FWM processes in a two-level system and a cascade three-level atomic system are theoretically and experimentally investigated. The relative intensities and polarization characteristics of the FWM signals in different laser polarization configurations and different level systems are experimentally investigated and compared. Also, the results are theoretically explained by different transition paths combinations. In the dressed-FWM processes, we study the dependence of dressing effect on the incident field’s polarization. The FWM signal generated by a linearly polarized pumping field is suppressed more by the dressing field than the one generated by a circularly polarized pumping field. However, an opposite effect was observed when the probe field’s polarization is changed. The multidressing mechanisms are used to explain these effects. In addition, the interference and polarization dependence of the coexisting FWM signals in the same atomic system are discussed.

© 2009 Optical Society of America

1. INTRODUCTION

The parametric four-wave mixing (FWM) is a useful process for generating coherent radiations from vacuum ultraviolet to infrared wavelengths. The polarization characteristics of two-photon resonant FWM processes have been investigated in several types of metal vapors gases. Tsukiyama [1] described polarization properties of the near-infrared FWM signal produced in Kr vapor, Museur et al. [2] studied the polarization dependence of the vacuum ultraviolet light generated by a four-wave sum-frequency generation process in Hg, and Ishii et al. [3] investigated polarization characteristics of FWM in NO gas. Besides producing coherent emissions, parametric FWM processes can also be used to study interference effects. Previous studies have used FWM processes to observe interference effects between different atomic polarizations [4, 5, 6]. Studies of interference effects in multilevel atomic systems have become an active field of research in recent years, which made it possible to coherently control the optical properties of atomic media [7, 8]. In parametric FWM processes, there are multiple quantum paths for each step of the nonlinear processes, and the probability amplitudes for these different transition paths are intimately related to the polarizations of the input laser fields. Therefore, it is possible to coherently control the nonlinear processes by manipulating the polarization states of incident laser beams.

In this paper, we report both theoretical and experimental results on the polarization dependence of the FWM signals generated in Na atomic vapor. Both two-level and three-level systems in Na atoms are used in these studies. The classical, as well as quantum, theoretical models have been developed to explain the dependence of the FWM signals on the polarization states of the incident laser beams. By comparing the FWM spectra for different laser polarization configurations, we can identify different contributions from third-order nonlinear susceptibility elements under different conditions. Furthermore, we explain the different contributions by the difference from combinations of transition paths for three incident beam polarization schemes. Moreover, we report the polarization characteristics of the singly dressed and doubly dressed FWM processes in either a two-level or a three-level atomic system in Na vapor. In the three-level atomic system the FWM signal generated by a linearly polarized pumping field is greatly suppressed by the dressing field, while the one generated by a circularly polarized pumping field is only slightly influenced by the dressing field. Also, different change rules are observed when the polarization of the probe field is changed. Different dressing effects of two dressing schemes are used to explain this phenomenon. The dressing effects, as well as the interference between the two coexisting FWM signals, have been discussed in different laser polarization configurations. Investigations of the interactions between different FWM processes and their polarization properties can help us to understand the underlying physical mechanisms and to effectively optimize the generated nonlinear optical signals. Controlling nonlinear optical processes can have many potential applications such as in all-optical switches [9] and quantum-information processing [10, 11].

This paper is organized as follows: Section 2 we describe our experimental setup. In Section 3 we present the basic theoretic treatments about Zeeman atomic subsystems interacting with arbitrarily polarized laser fields. We will discuss the experimental results and comparisons with the theoretical calculations in Section 4. Section 6 summarizes main results and gives conclusions.

2. EXPERIMENTAL SETUP

The experiments are carried out in Na vapor (in a heat pipe oven), which is heated up to a temperature of about 235°C. Three energy levels from Na atoms are involved in the experimental schemes. As shown in Fig. 1 , energy levels |0(3s12) and |1(3p32) form the two-level atomic system. Two laser beams Ed (ωp, kd, and Rabi frequency Gd) and Ed (ωp, kd, and Rabi frequency Gd), connecting the transition between |0⟩ and |1⟩, propagate in the opposite direction of the weak probe beam Ep (ωp, kp, and Rabi frequency Gp), which also connects the transition between |0⟩ and |1⟩. The three laser beams come from the same dye laser DL1 (wavelength of 589.0nm, 10Hz repetition rate, 5ns pulse width, and 0.04cm1 linewidth) with the frequency detuning Δ1, pumped by the second-harmonic beam of a Nd:YAG laser. These three laser fields generate a degenerate-FWM (DFWM) process satisfying the phase-matching condition of ks1=kp+kdkd. The energy levels |0(3s12)|1(3p32)|2(4d32) form the cascade three-level atomic system. Two additional coupling laser beams Ec (ωc, kc, and Rabi frequency Gc) and Ec (ωc, kc, and Rabi frequency Gc), connecting the transition between |1⟩ to |2⟩ are from another dye laser DL2 (which has the same characteristics as the DL1) with a frequency detuning Δ2. Ec, Ec, and Ep fields interact with each other and generate a nondegenerate FWM (NDFWM) signal, satisfying the phase-matching condition of ks2=kp+kckc. The generated DFWM and NDFWM signals propagate along slightly different directions due to their different spatial phase-matching conditions. Two photomultiplier tube (PMT) detectors are used to receive the horizontally polarized component (P polarization) and the vertically polarized component (S polarization) for one of the signal beams, or horizontally polarized components of both signal beams, respectively. A half-wave plate (HWP) and a quarter-wave plate (QWP) are selectively used (in different experiments, respectively) to control the polarization states of the incident fields. The generated FWM signals may pass through another HWP and a polarization beam splitter (PBS) before being detected by the two PMTs.

3. BASIC THEORY

3A. Various Nonlinear Susceptibilities for Different Polarization Schemes

The polarization dependence of the FWM signals can be explained using either a classical or quantum mechanical description [12]. Classically, the FWM signal intensity is proportional to the square of the atomic polarization induced in the medium. For example, as for phase-conjugated FWM generation in the cascade atomic system at frequency ωs=ωcωc+ωp (as shown in Fig. 1, with beams kd and kd blocked), the nonlinear polarization along i (i=x,y) direction is given by

Pi(3)(ωs)=ϵ0jklχijkl(3)(ωs;ωc,ωc,ωp)Ecj(ωc)Eck*(ωc)Epl(ωp),
where χijkl(3)(ωs;ωc,ωc,ωp) is the tensor component of the third-order nonlinear susceptibility. For an isotropic medium like Na atomic vapor and considering that all the incident beams and signals are transverse waves, only four nonzero tensor elements are involved in this system, which are denoted as χxxxx, χyxxy, χyyxx, χyxyx. Different polarization configurations of the incident fields can involve different nonlinear susceptibility elements. For example, when we use a HWP to change the polarization of the Ep field while the other two beams are originally polarized in the horizontal direction, the probe field will have two perpendicular components: Epx=EpCos2θ and Epy=EpSin2θ (θ is the rotated angle of the HWP’s axis from the x axis). Consequently, the polarization has two corresponding components, i.e., horizontal component Px(3)(ωs)=ϵ0χxxxx|Ec|2|Epx| and perpendicular component Py(3)(ωs)=ϵ0χyxxy|Ec|2|Epy|. Then the effective susceptibility elements χx and χy are defined as χx=χxxxxcos2θ and χy=χyxxysin2θ. As for the other two cases with kc and kc modulated by a HWP. χyyxx and χyxyx become dominant on generating FWM signals polarized in the S direction (the signals in the P direction for the three cases are all generated by χxxxx). The microscopic mechanism of nonlinear different susceptibilities will be discussed in Subsection 3B.

If a QWP is used to modulate the incident beams, the effective nonlinear susceptibilities will be different while the excited susceptibilities are the same as in the corresponding cases with HWP modulation. Table 1 presents all the effective susceptibilities for the three-field polarization schemes.

In order to measure the polarization states of the FWM signals, a HWP and a PBS are placed in the path of the signal beam (as shown in Fig. 1). When an arbitrarily polarized field (EyeiδEx) passes through the HWP+PBS combination, the detected intensities are

Ix=cos22α|Ex|2+|Ey|2sin22α+|Ex||Ey|sin4αcosδ,
Iy=sin22α|Ex|2+|Ey|2cos22α|Ex||Ey|sin4αcosδ,
respectively, where α is the rotation angle of the HWP from the x axis and δ is the phase difference between the two polarization [horizontal (x) and vertical (y)] components of the signal beam.

3B. Nonlinear Susceptibilities for a Zeeman-Degenerate System Interacting with Polarized Fields

The polarization dependence of the FWM signals can also be described by the semi-classical treatment. It is based on the fact that there are different transition paths combinations consisting of various transitions between Zeeman sublevels for different polarization schemes [as shown in Fig. 2 ]. According to the experimental setup, the x axis is the original polarization direction of all the incident fields, and it is also the quantization axis. We then decompose the arbitrary field into two components: parallel to and perpendicular to the x axis, respectively. When this field interacts with atoms, the perpendicular component can be decomposed into equally left-circularly- and right-circularly-polarized components. Different polarization schemes can excite different transition paths in the Zeeman-degenerate atomic systems, and so it is necessary to take into account the Clebsch–Gordan coefficients associated with the various transitions between Zeeman sublevels in all pathways when calculating the FWM intensities. Figure 2 shows the transition schematic configurations for the Zeeman-degenerate two-level and three-level cascade systems interacting with one arbitrarily polarized and two horizontally polarized fields. Table 2, 3 list all the perturbation chains for different cases, respectively. By considering the schematic figures and the tables, we can obtain the expressions of various density matrices corresponding to nonlinear susceptibilities for different polarization schemes.

Figure 2a shows the configuration of generating the FWM signals in P-polarization (represented as χxxxx) in the two-level system. It contains two sub-two-level systems: |a12|b12 and |a12|b12. The respective perturbation chains are listed in Table 2 and the total contribution of these chains to the density-matrix element that induces the FWM signal in the P-polarization direction is

ρ̃p(3)=iM=±12|GdM0|2GpM0(1(iΔp+ΓbMaM)2+1Δp2+ΓbMaM2)(1ΓaMaM+1ΓbMbM).
Then from χxxxx=Nμρp(3)ϵ0|Ec|2Ep, we can get χxxxx.

Figure 2b presents the configuration for generating the S-polarized FWM signals when the waveplate (WP) changes kp (corresponds susceptibility χyxxy). It contains two right-circularly-polarized V-type subsystems (|a12|b12|b12 and |a12|b32|b12), two left-circularly-polarized V-type subsystems (|a12|b32|b12 and |a12|b12|b12), one right-circularly-polarized reversed V-type subsystem |a12|b12|a12 and one left-circularly-polarized RV-type subsystem |a12|b12|a12. Their perturbation chains are listed in Table 2 and the total density-matrix element including contributions from all the perturbation chains can be written as

ρ̃s1(3)=[iGp12|Gd120|2(iΔp+Γb12a12)2Γa12a12+iGp12+|Gd120|2(iΔp+Γb12a12)2Γa12a12]M=±122ΓbMaM|GdM0|2ΓaMaM(Δp2+ΓbMaM2)[iGpM+(iΔp+ΓbM+1aM)+iGpM(iΔp+ΓbM1aM)].

When the polarization of the kd field is changed by the WP, the subsystems generating FWM signals in the P-polarization direction and their expressions are the same as the ones for changing the kp field. However, the configuration of generating the S-polarized FWM signal, as shown in Fig. 2c, contains two left-circularly-polarized V-type subsystems (|a12|b12|b32 and |a12|b12|b12), two right-circularly-polarized V-type subsystems (|a12|b12|b12 and |a12|b12|a32), and one right-circularly-polarized RV-type subsystem (|a12|a12|b12), and one left-circularly-polarized RV-type subsystem (|a12|a12|b12). The total contribution to the third-order nonlinear density-matrix element is

ρ̃s2(r)=iGp120Gd12+(Gd120)*Γa12a12(iΔp+Γb12a12)(iΔp+Γb12a12)iGp120Gd12(Gd120)*Γa12a12(iΔp+Γb12a12)(iΔp+Γb12a12)M=±12iGpM0(GdM0)*ΓaMaM(iΔp+ΓbMaM)[GdM(iΔp+ΓbM1aM)+GdM+(iΔp+ΓbM+1aM)].
Then we can obtain the nonlinear susceptibility element χxyxy.

When changing the polarization of kd field, as shown in Fig. 2d, there are four perturbation chains as listed in Table 2. The total contribution from all the perturbation chains to the third-order nonlinear density-matrix element can be written as

ρ̃s3(3)=4iGp120Gd120(Gd12)*Γa12a12(iΔp+Γb12a12)(iΔp+Γb12a12).
This expression is simpler due to the symmetry of the configuration relative to M=0. Then, we can obtain element χxxyy.

For the three-level cascade-type (C3-type) system, the schematic charts are shown in Figs. 2e, 2f, 2g, 2h [with dressing fields kd and kd blocked], which change kp, kc, and kc fields. The corresponding perturbation chains are listed in Table 3. The expressions of the corresponding third-order nonlinear density-matrix elements are

ρp(3)=M=±12iGpM0iGcM(GcM0)*(iΔp+ΓbMaM)2[i(Δc+Δp)+ΓcMaM],
ρs1(3)=M=±12iGpM|GcM0|2(iΔp+ΓbM1aM)2([i(Δc+Δp)+ΓcM1aM])M=±12iGpM+|GcM0|2(iΔp+ΓbM+1aM)2[i(Δc+Δp)+ΓcM+1aM],
ρs2(3)=M=±12iGpM0(GcM0)*(iΔp+ΓbMaM)×[iGcM+(iΔp+ΓbM+1aM)[i(Δc+Δp)+ΓcM+1aM]+iGcM(iΔp+ΓbM1aM)[i(Δc+Δp)+ΓcM1aM]],
ρs3(3)=M=±12iGpM0GcM0(iΔp+ΓbMaM)[i(Δc+Δp)+ΓcMaM]((GcM)*iΔp+ΓbM1aM+(GcM+)*iΔp+ΓbM+1aM).

3C. Third-Order Density-Matrix Elements in the Presence of Dressing Fields

For the case with a single dressing by the kd field (with kd blocked), the density-matrix elements of the dressed FWM signals (generated in the C3 system) are given by

ρbMaM(3)=iGpM0|GcM0|2(i(Δc+Δp)+ΓcMaM)×1(iΔp+ΓbMaM+|GdM|2i(ΔpΔd)+ΓaMaM+|GpM0|2ΓaMaM+|GcM0|2i(Δc+Δp)+ΓcMaM)2,(M=±12).
For the case of double dressing (with kd and kd both on), the third-order nonlinear density-matrix elements can be written as
ρbMaM(3)=iGpM0|GcM0|2i(Δc+Δp)+ΓcMaM×1(iΔp+ΓbMaM+2|GdM|2i(ΔpΔd)+ΓaMaM+|GpM0|2ΓaMaM+|GcM0|2i(Δc+Δp)+ΓcMaM)2,(M=±12).
One can easily see that the multidressed fields appear in the denominator and the dressing effect is mainly caused by the strong dressing field Gd. The other two fields, however, can enhance or suppress such dressing effect. In fact, the coupling field Gc, which is denoted as sequential with Gd, generally enhances the dressed effect induced by Gd, while the probe field Gp, which is denoted as nested with Gd, generally suppresses the dressing effect [13].

4. RESULTS AND DISCUSSIONS

First, we use a HWP to modulate the polarization of one of the incident beams, while the other two beams are kept to be in horizontally polarization. In this case, the incident beams are all linearly polarized. Figures 3a, 3b show the relative FWM intensities in the P and S polarizations, respectively, in the cascade three-level atomic system with respect to the rotation angle θ of the HWP. From Table 1 we can see that, for the horizontally polarized component [Fig. 3a], the dependence of the FWM intensity on θ follows (cos2θ)2 while the vertically polarized component obeys (sin2θ)2 (represented by the solid curves in Fig. 3). This means that the FWM signals are linearly polarized. Similar results have been reported in other systems [2, 4, 6]. From Fig. 3b, the signal amplitudes are different for the three laser polarization configurations, which can be attributed to different contributions from the third-order nonlinear susceptibility elements under different conditions. As discussed in Section 3, different polarization schemes of incident fields can excite different nonlinear susceptibilities, and they can have different quantum transition paths. When the kp field is modulated by the HWP, χyxxy is excited, which generates FWM signal in the S-polarization direction. In the other two cases, both the kc and kc fields are modulated, so both χyyxx and χyxyx are respectively stimulated. The signal amplitudes indicate different contributions from third-order nonlinear susceptibility elements for three different laser polarization schemes.

Figures 3c, 3d depict the polarization dependences of the FWM signals on the rotation angle of the QWP in the two-level DFWM process. First, the probe beam kp is elliptically polarized and the ellipticity is controlled by the QWP, while the other beams have linear polarization along the x axis [the square points in Figs. 3c, 3d]. In Figs. 3c, 3d, the experimental results are well described by the functions sin4φ+cos4φ and 2(sinφcosφ)2 (the solid curves), respectively. If one of the incident beams is elliptically polarized, the generated FWM signal is also elliptically polarized, which is in good agreement with the theoretical prediction. Comparing the vertically polarized intensities of the signal beams [Figs. 2b, 2d], there are different ratios of oscillation amplitudes. It indicates that the ratios of the third-order nonlinear susceptibility elements are different for the cascade three-level system and the two-level system, which are well described by Eq. (8).

To detect the polarization states of the FWM signals, we place a HWP+PBS combination as a polarization analyzer in the generated FWM signal beam (as shown in Fig. 1). In fact, when a QWP is used to modulate the kc field’s polarization (or ellipticity ϵ), the polarizations of the FWM signals are also changed. Besides, the excited nonlinear susceptibilities of the P and S polarizations greatly modify the signal’s polarization states, which can be detected by the HWP+PBS combination. Figure 4 presents the detected results. Each curve is obtained by rotating the HWP while keeping the QWP in the path of the kc field fixed. In this case, |Ex|χxxxxsin4θ+cos4θ and |Ey|χyyxxsin2θcos2θ. According to Eqs. (2, 3), the detected intensities should be

Ix=χxxxx2(cos4θ+sin4θ)cos22α+χyyxx2(2sin2θcos2θ)sin22α+χxxxxχyyxx(cos4θ+sin4θ)(2sin2θcos2θ)sin4αcosδ,
Iy=χxxxx2(cos4θ+sin4θ)sin22α+χyyxx2(2sin2θcos2θ)cos22αχxxxxχyyxx(cos4θ+sin4θ)(2sin2θcos2θ)sin4αcosδ.
If the kc field is linearly polarized (θ=0, ϵ=1, the square points in Fig. 4), the NDFWM signal is also linearly polarized, and the horizontal (x) and vertical (y) signal intensities obey the relations of χxxxx2cos22α and χxxxx2sin22α, respectively. When the polarization of the kc field is changed, the other nonlinear susceptibility components are excited and the FWM signal is then elliptically polarized. From Fig. 4 we can see that, if the kc field is either elliptically (θ=30°, ϵ=0.5, the triangle points) or circularly (θ=45°, ϵ=0, asterisk points) polarized, the NDFWM signals are also elliptically polarized. This can be confirmed by Eq. (11). When the input kc field is circularly polarized, the FWM signal can be circularly polarized once the condition χxxxx=χyyxx is satisfied.

Figure 5 shows the dependence of the dressed FWM signal on the polarization of the kc field. Figures 5a, 5b depict the results for the kd singly-dressed and kd and kd doubly dressed FWM signals, respectively, for three different ellipticities of the kc field. The dressing fields kd and kd are both linearly polarized along the x axis. Comparing to Fig. 4a, the reduction of the signal intensity is more than 50%. More interestingly, the FWM signals generated by the linearly polarized kc field [the square points in Fig. 4a and Fig. 5a] are greatly suppressed by the kd dressing field while the FWM signals generated by the circularly polarized kc field [the asterisk points in Fig. 4a and Fig. 5a] are only slightly suppressed by the kd dressing field. So, in Fig. 5a the square points are lower than the other curves, which is opposite to the case in Fig. 4a. Figure 5c presents the dependences of the pure FWM and dressed FWM signal intensities on the ellipticity of the kc field. The square points represent pure FWM case, which decreases as the kc’s ellipticity reduces [from 1 to 0 when the QWP is rotated from 0to45  degrees]. The dot points represent the singly dressed FWM case, which shows an opposite variation from the pure FWM. This result can be explained by the expression [Eq. (9)] for the dressed FWM case. In the denominator of Eq. (9), Gd’s sequential dressing field Gc can enhance the dressing effect. When the coupling field is linearly polarized, its Rabi frequency Gc in the denominator is at its maximum, so the dressing effect is strongest [square points in Fig. 5a] and the FWM signal is lowest.

Moreover, comparing the singly dressed and doubly dressed FWM signals, they have similar suppressed intensities when the signals are linearly polarized. However, when the signals are elliptically polarized, the suppression in the doubly dressed case is stronger than in the singly dressed case. In order to explain this effect, mutual-dressing processes and constructive or destructive interference between the two coexisting FWM channels should be considered [14, 15]. According to Eqs. (9, 10), if one only considers the dressing effect, the FWM intensity should be further suppressed in the doubly dressed configuration. However, as can be seen from Fig. 1, when five laser beams are all on, the DFWM signal ks1 and the NDFWM signal ks2 coexist in the experiment, and these two FWM signals overlap in frequency and the angle between their propagation directions is very small. As mentioned above, if the incident beams are all linearly polarized, the generated FWM signals are linearly polarized also, so constructive or destructive interference can occur in this system. Such interferences between two FWM processes in the two-level and three-level atomic systems can generate entangled photon pairs [16, 17]. Constructive or destructive interference can be controlled by the phase difference between the two FWM processes, which can be varied by adjusting the detuning difference Δ(Δ=Δ1Δ2) between the incident laser beams. By varying the detuning difference Δ from 0 to very certain values, the phase difference between the two FWM processes alters from in-phase to out-phase, so the interference can switch back and forth between constructive and destructive values [18, 19, 20]. In this case, the observed experimental data include two contributions: the dressing effect and the interference effect. However, when the kc field is elliptically or circularly polarized, the NDFWM signal ks2 is elliptically polarized, but the DFWM signal ks1 is still linearly polarized. In this case, the doubly dressed effect plays a dominant role to further suppress the intensity of the generated FWM signal.

The dependences of the dressing effects on the polarization of the probe field are shown in Fig. 6 . Compared to Fig. 5a, the linearly polarized signal (square points) is higher than the other curves even though it is also dressed. Such opposite behaviors in changing the pumping field kc and the probe field kp can be accounted for by Eq. (9). In the denominator of the equation, the dressing field Gd and the coupling field Gc are in summation form, which is called sequential-dressing scheme, and Gd and Gp are in the nest-dressing scheme [13]. According to the interaction properties of the two dressing schemes, the sequentially dressing Gc field controls the FWM process directly, which can enhance the Gd dressing effect. When the coupling field is linearly polarized, the Rabi frequency Gc in the denominator is at its maximum, so the dressing effect is strongest [square points in Fig. 5a]. As Gp is nested with Gd, it controls the FWM process only indirectly and it often suppresses the Gd dressing effect, so for the linearly polarized kp field, the signal [square points in Fig. 6b] is higher than the other curves.

Figure 7a depicts the dependence of the horizontal intensity of the FWM signal on α generated in the two-level system when the probe beam kp is modulated by the HWP. In this case, the generated FWM signals are linearly polarized (δ=0), with |Ex|χxxxxcos2θ and |Ey|χyxxysin2θ. From Fig. 7a, with a rotating HWP, the maximal values of the curves are shifted, which indicates that the polarization of the FWM signal changes with that of the probe beam. Previous experiment [4] in rubidium vapor has shown that the polarizations of the driving field and the signal wave are identical and collinear.

If the signal and the probe beams are polarized along the same direction, a maximum signal intensity is observed when the two HWPs are rotated to be at the same angle [that is, α=θ, the solid line in Fig. 7c]. The experimental results (the scattered points) in Fig. 7c present a big difference from the solid theoretical line, which suggests that the signal and the probe beams have different polarization directions. According to Eqs. (2, 3), the polarization of the FWM signal is dependent on the ratio χyxxyχxxxx. If χyxxy=χxxxx, the signal and the probe beams would have polarization along the same direction. However, our theoretical expressions [Eq. (4) and Eq. (5)], indicate that χyxxyχxxxx, so the signal and the probe beams have different polarization directions.

Figure 7b presents the kc singly dressed (the square points) and kc and kc doubly dressed (the dot points) DFWM signals when the input beams (kd, kd, kp, kc, and kc) are all horizontally polarized. Compared with the pure-FWM signal [the square points in Fig. 7a], the two FWM signals dressed by either kc or kc and kc are both significantly suppressed and have similar suppressed intensities. As discussed above, for the kc and kc doubly dressed FWM process, the mutual-dressing effect and constructive or destructive interference should also be considered simultaneously.

5. CONCLUSION

The polarization dependences of the DFWM and NDFWM processes, and their dressing effects in two-level and three-level cascade-type atomic systems are investigated experimentally and theoretically. The effective nonlinear susceptibilities and the corresponding combinations of different transition paths for various laser polarization configurations are analyzed in detail. The polarizations of the generated FWM signals depend on both the input laser polarizations and the excited nonlinear susceptibility elements of the atomic systems. In the singly dressed FWM processes, we found that the dependences of dressing effects on the polarizations of the pumping and probe fields are very different. The FWM signal generated by the linearly polarized pumping field kc is strongly dressed by the kd field while the FWM signal generated by the circularly polarized kc is weakly dressed by the kd field, but the opposite behavior was seen for changing the polarization of the probe field. Such behavior is attributed to different dressing effects of the sequential-dressing scheme and the nest-dressing scheme. For the doubly dressed process, the polarization dependence of the signal intensity is also investigated. It is found that when the two coexisting FWM signals have the same polarization, the suppressed intensities of the singly dressed and doubly dressed signals are similar. In this case, both the mutual-dressing effects and the constructive or destructive interference should be considered simultaneously. However, when the two FWM signals have different polarizations, the doubly dressed effect plays a dominant role, so the doubly dressed signals are further suppressed. Studying polarization dependence of the FWM processes in multilevel atomic systems can be very important in optimizing and controlling nonlinear optical processes, and for various potential applications in nonlinear signal processing.

ACKNOWLEDGMENTS

This work was supported by the National Natural Science Foundation of China (NSFC) (No. 60678005), the Foundation for the Author of National Excellent Doctoral Dissertation of China (No. 200339), the Specialized Research Fund for the Doctoral Program of Higher Education of China (No. 20050698017), the Fok Ying-Tong Education Foundation for Young Teachers in the Institutions of Higher Education of China (No. 101061), and the Program for New Century Excellent Talents in University (NCET-08–0431).

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Table 1. Effective Nonlinear Susceptibilities for Different Laser Polarization Configurations

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Table 2. Perturbation Chains of the Two-Level System for Different Laser Polarization Configurations

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Table 3. Perturbation Chains of the Cascade System for Different Laser Polarization Configurations

 figure: Fig. 1

Fig. 1 Schematic diagrams of the experimental arrangement and the relevant energy levels in the Na atom.

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 figure: Fig. 2

Fig. 2 Energy level diagrams and transition paths at different laser polarization configurations. (a) and (e) Schematic diagrams of the P-polarization generation in two-level and three-level systems when the waveplates change kp, kd, and kd. (b)–(d) and (f)–(h) Schematic diagrams of S-polarization generation in two-level and three-level systems when the waveplates change kp, kd, and kd, respectively. Dotted, long-dashed, solid, and short-dashed lines are transitions for the probe, coupling, dressing, and FWM signal fields, respectively.

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 figure: Fig. 3

Fig. 3 Variations of the relative FWM intensities versus the rotation angle of the waveplate. (a) and (b) The FWM signals of the cascade three-level system with the HWP. (c)–(d) The FWM signals of the two-level system with the QWP. The scattered points are the experimental data and the solid curves are the theoretical results.

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 figure: Fig. 4

Fig. 4 Dependence of the relative NDFWM signal intensity on α for three values of the coupling laser’s ellipticity.

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 figure: Fig. 5

Fig. 5 Variations of the dressed NDFWM signal intensities versus α. (a) Singly dressed FWM signals when the coupling beam kc is modulated by the QWP. (b) Doubly dressed FWM signals when the coupling beam kc is modulated by the QWP. (c) Variation of the relative FWM intensity versus the rotation angle θ of the QWP.

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 figure: Fig. 6

Fig. 6 Dependence of the relative NDFWM signal intensity on α for three values of probe laser’s ellipticity. (a) and (b) Pure and singly dressed FWM signals, respectively, of the cascade three-level system as the probe beam is modulated by the QWP.

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 figure: Fig. 7

Fig. 7 Variations of the DFWM signal intensities versus α (a) Pure FWM signal of the two-level system versus α for several different rotation angles θ of the HWP. (b) Singly dressed and doubly dressed FWM signals when the input beams are all horizontally polarized. (c) The rotation angle α of the polarization analyzer when the maximum intensity is observed. The scattered points are the experimental results, and the solid line represents the case with the polarization analyzer and polarizer rotating the same angle (α=θ).

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Figures (7)

Fig. 1
Fig. 1 Schematic diagrams of the experimental arrangement and the relevant energy levels in the Na atom.
Fig. 2
Fig. 2 Energy level diagrams and transition paths at different laser polarization configurations. (a) and (e) Schematic diagrams of the P-polarization generation in two-level and three-level systems when the waveplates change k p , k d , and k d . (b)–(d) and (f)–(h) Schematic diagrams of S-polarization generation in two-level and three-level systems when the waveplates change k p , k d , and k d , respectively. Dotted, long-dashed, solid, and short-dashed lines are transitions for the probe, coupling, dressing, and FWM signal fields, respectively.
Fig. 3
Fig. 3 Variations of the relative FWM intensities versus the rotation angle of the waveplate. (a) and (b) The FWM signals of the cascade three-level system with the HWP. (c)–(d) The FWM signals of the two-level system with the QWP. The scattered points are the experimental data and the solid curves are the theoretical results.
Fig. 4
Fig. 4 Dependence of the relative NDFWM signal intensity on α for three values of the coupling laser’s ellipticity.
Fig. 5
Fig. 5 Variations of the dressed NDFWM signal intensities versus α. (a) Singly dressed FWM signals when the coupling beam k c is modulated by the QWP. (b) Doubly dressed FWM signals when the coupling beam k c is modulated by the QWP. (c) Variation of the relative FWM intensity versus the rotation angle θ of the QWP.
Fig. 6
Fig. 6 Dependence of the relative NDFWM signal intensity on α for three values of probe laser’s ellipticity. (a) and (b) Pure and singly dressed FWM signals, respectively, of the cascade three-level system as the probe beam is modulated by the QWP.
Fig. 7
Fig. 7 Variations of the DFWM signal intensities versus α (a) Pure FWM signal of the two-level system versus α for several different rotation angles θ of the HWP. (b) Singly dressed and doubly dressed FWM signals when the input beams are all horizontally polarized. (c) The rotation angle α of the polarization analyzer when the maximum intensity is observed. The scattered points are the experimental results, and the solid line represents the case with the polarization analyzer and polarizer rotating the same angle ( α = θ ) .

Tables (3)

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Table 1 Effective Nonlinear Susceptibilities for Different Laser Polarization Configurations

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Table 2 Perturbation Chains of the Two-Level System for Different Laser Polarization Configurations

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Table 3 Perturbation Chains of the Cascade System for Different Laser Polarization Configurations

Equations (15)

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P i ( 3 ) ( ω s ) = ϵ 0 j k l χ i j k l ( 3 ) ( ω s ; ω c , ω c , ω p ) E c j ( ω c ) E c k * ( ω c ) E p l ( ω p ) ,
I x = cos 2 2 α | E x | 2 + | E y | 2 sin 2 2 α + | E x | | E y | sin 4 α cos δ ,
I y = sin 2 2 α | E x | 2 + | E y | 2 cos 2 2 α | E x | | E y | sin 4 α cos δ ,
ρ ̃ p ( 3 ) = i M = ± 1 2 | G d M 0 | 2 G p M 0 ( 1 ( i Δ p + Γ b M a M ) 2 + 1 Δ p 2 + Γ b M a M 2 ) ( 1 Γ a M a M + 1 Γ b M b M ) .
ρ ̃ s 1 ( 3 ) = [ i G p 1 2 | G d 1 2 0 | 2 ( i Δ p + Γ b 1 2 a 1 2 ) 2 Γ a 1 2 a 1 2 + i G p 1 2 + | G d 1 2 0 | 2 ( i Δ p + Γ b 1 2 a 1 2 ) 2 Γ a 1 2 a 1 2 ] M = ± 1 2 2 Γ b M a M | G d M 0 | 2 Γ a M a M ( Δ p 2 + Γ b M a M 2 ) [ i G p M + ( i Δ p + Γ b M + 1 a M ) + i G p M ( i Δ p + Γ b M 1 a M ) ] .
ρ ̃ s 2 ( r ) = i G p 1 2 0 G d 1 2 + ( G d 1 2 0 ) * Γ a 1 2 a 1 2 ( i Δ p + Γ b 1 2 a 1 2 ) ( i Δ p + Γ b 1 2 a 1 2 ) i G p 1 2 0 G d 1 2 ( G d 1 2 0 ) * Γ a 1 2 a 1 2 ( i Δ p + Γ b 1 2 a 1 2 ) ( i Δ p + Γ b 1 2 a 1 2 ) M = ± 1 2 i G p M 0 ( G d M 0 ) * Γ a M a M ( i Δ p + Γ b M a M ) [ G d M ( i Δ p + Γ b M 1 a M ) + G d M + ( i Δ p + Γ b M + 1 a M ) ] .
ρ ̃ s 3 ( 3 ) = 4 i G p 1 2 0 G d 1 2 0 ( G d 1 2 ) * Γ a 1 2 a 1 2 ( i Δ p + Γ b 1 2 a 1 2 ) ( i Δ p + Γ b 1 2 a 1 2 ) .
ρ p ( 3 ) = M = ± 1 2 i G p M 0 i G c M ( G c M 0 ) * ( i Δ p + Γ b M a M ) 2 [ i ( Δ c + Δ p ) + Γ c M a M ] ,
ρ s 1 ( 3 ) = M = ± 1 2 i G p M | G c M 0 | 2 ( i Δ p + Γ b M 1 a M ) 2 ( [ i ( Δ c + Δ p ) + Γ c M 1 a M ] ) M = ± 1 2 i G p M + | G c M 0 | 2 ( i Δ p + Γ b M + 1 a M ) 2 [ i ( Δ c + Δ p ) + Γ c M + 1 a M ] ,
ρ s 2 ( 3 ) = M = ± 1 2 i G p M 0 ( G c M 0 ) * ( i Δ p + Γ b M a M ) × [ i G c M + ( i Δ p + Γ b M + 1 a M ) [ i ( Δ c + Δ p ) + Γ c M + 1 a M ] + i G c M ( i Δ p + Γ b M 1 a M ) [ i ( Δ c + Δ p ) + Γ c M 1 a M ] ] ,
ρ s 3 ( 3 ) = M = ± 1 2 i G p M 0 G c M 0 ( i Δ p + Γ b M a M ) [ i ( Δ c + Δ p ) + Γ c M a M ] ( ( G c M ) * i Δ p + Γ b M 1 a M + ( G c M + ) * i Δ p + Γ b M + 1 a M ) .
ρ b M a M ( 3 ) = i G p M 0 | G c M 0 | 2 ( i ( Δ c + Δ p ) + Γ c M a M ) × 1 ( i Δ p + Γ b M a M + | G d M | 2 i ( Δ p Δ d ) + Γ a M a M + | G p M 0 | 2 Γ a M a M + | G c M 0 | 2 i ( Δ c + Δ p ) + Γ c M a M ) 2 , ( M = ± 1 2 ) .
ρ b M a M ( 3 ) = i G p M 0 | G c M 0 | 2 i ( Δ c + Δ p ) + Γ c M a M × 1 ( i Δ p + Γ b M a M + 2 | G d M | 2 i ( Δ p Δ d ) + Γ a M a M + | G p M 0 | 2 Γ a M a M + | G c M 0 | 2 i ( Δ c + Δ p ) + Γ c M a M ) 2 , ( M = ± 1 2 ) .
I x = χ x x x x 2 ( cos 4 θ + sin 4 θ ) cos 2 2 α + χ y y x x 2 ( 2 sin 2 θ cos 2 θ ) sin 2 2 α + χ x x x x χ y y x x ( cos 4 θ + sin 4 θ ) ( 2 sin 2 θ cos 2 θ ) sin 4 α cos δ ,
I y = χ x x x x 2 ( cos 4 θ + sin 4 θ ) sin 2 2 α + χ y y x x 2 ( 2 sin 2 θ cos 2 θ ) cos 2 2 α χ x x x x χ y y x x ( cos 4 θ + sin 4 θ ) ( 2 sin 2 θ cos 2 θ ) sin 4 α cos δ .
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