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A wide range of photonic crystal fibers (PCFs) [1], [2] can be used as potential waveguides and devices which may exploit their characteristics of being single moded, having higher modal birefringence, and offering adjustable spot-size and dispersion properties, which may be tailored for various linear and nonlinear applications. Initially, PCF was considered to be an endlessly single mode fiber (SMF), but later, numerical studies such as using the multipole method and the finite element method (FEM), have revealed that the cutoff conditions are critically controlled by the diameter to pitch ratio [3], [4], [5]. Their mode field areas (MFAs) are controllable and thus able to achieve both large and small spot-sizes. As an example, PCFs with smaller MFAs can be envisaged by enhancing their power density and tailoring their dispersion properties for various nonlinear applications, such as supercontinuum generation. Such a PCF with small core can also allow easy access to the evanescent fields for the design of optical sensors.

However, practical difficulties related to achieving efficient coupling of a PCF with a smaller MFA to the input/output sections have often been considered as creating a serious drawback in PCF technology. Unlike fusion splicing in conventional SMF, joining a PCF is difficult as the integrity of the air holes is difficult to preserve, even though several recent efforts concerning fusion splicing of a PCF to an SMF have been reported [6], [7], [8]. However, to obtain a low-loss coupling is particularly challenging due to the large mismatch between the MFA of a PCF and that of an SMF. A short gradient index fiber lens has also been considered [9] by incorporating this component between the two coupling sections with different MFAs. Use of a fused biconical taper, which is often used for a passive fiber coupler, has also been envisaged by placing a PCF and a pretapered SMF side by side and twisting and tapering them for efficient evanescent coupling [10]. A PCF can also be tapered adiabatically to adjust its MFA [11], [12]. As an example, if the up-tapered part has a larger width near the end, its MFA increases, and the coupling loss to an SMF can be relatively low, as reported in the literature [13], [14]. However, these terminal sections with a large core dimension are likely to be multimoded which could also restrict the flexibility of the PCF designs. On the other hand, if the dimensions of a tapered PCF are adiabatically reduced, when the core mode approaches cutoff, the MFA would also increase. PCFs have been routinely tapered to control their dispersion properties with their pitch reduced from 3.0 Formula$\mu\hbox{m}$ to 500 nm [15], and even below 300 nm [16].

When a PCF is operating near the cutoff condition, as the pitch is reduced, this leads to the expansion of the mode field into the air cladding region [17]. This could expand the MFA to a size similar to that of an SMF which would make coupling between them easier. For this purpose, a PCF section can be tapered to bring it close to the cutoff condition. However, as it expands very rapidly in this region, it may be difficult to control as any small fabrication errors can make the MFA unstable when it expands exponentially. A similar problem exists in coupling a laser beam with a small asymmetric shape to an SMF with a larger circular beam profile. In that context, monolithically integrated spot-size converters (SSCs) have been reported [18], [19] and have been designed to transform the spot-size of the output laser beam to allow for efficient coupling. To control the MFA with its fabrication tolerances, it is suggested here, for the first time, that a secondary guide can be considered. This approach is evaluated by using a rigorous full-vectorial FEM and the Least Squares Boundary Residual (LSBR) method. It is also shown here that the MFA can be stabilized, this being to account for the changes that may occur during the manufacturing processes of a tapered PCF. Coupling between waveguide sections with different spot-sizes have been a consistent problem, such as for photonic crystals [20], plasmonic waveguides [21], [22] as well as for efficient light extraction [23], [24], where the approach presented here, i.e., the use of tapered guided wave section, can be considered.

1.1. Theory

The coupling losses are caused by the mismatch of the MFAs and changes in the effective indices between the coupling sides. A typical approach to reduce the coupling loss would be to transform the MFA of one side adiabatically to achieve a better matching. If the changes are implemented slowly compared to the diffraction angle then the terminal MFA would give a clear indication of coupling efficiency enhancement. Hence, an accurate mode solver could be used to find the MFA of a tapered PCF rather than a beam evolutionary approach [10], [13] or a time-domain approaches [12], which are computationally more expensive.

In the modal solution approach based on the FEM, the intricate cross section of the PCF can be accurately represented using many triangles of different shapes and sizes [25], [26]. This flexibility makes the FEM preferable when compared with the finite difference method (FDM), which not only uses inefficient regular spaced meshing but, in addition, cannot represent slanted or curved dielectric interfaces. The optical modes in a high contrast PCF, with 2-D confinement, are also hybrid in nature, with all six components of the Formula${\bf E}$ and Formula${\bf H}$ fields being present. It is also known that modal hybridness is enhanced by the presence of slanted or curved dielectric interfaces. Hence, only a vectorial formulation can accurately represent their modal solutions and also the need for an accurate representation of the circular air holes. In the present approach, a Formula${\bf H}$-field based rigorous full-vectorial FEM has been used to analyze the operation regime of PCFs with air holes arranged in a triangular lattice in the silica cladding. The Formula${\bf H}$-field formulation [25] with the augmented penalty function technique is given as Formula TeX Source $$\omega^{2} = {\left(\int(\nabla \times \vec{\bf H})^{\ast} \cdot \mathhat{\varepsilon}^{-1}(\nabla \times \vec{\bf H})\,d\Omega\right) + \left(\int(\alpha/\varepsilon_{o})(\nabla \cdot \vec{\bf H}) \ast (\nabla \cdot \vec{\bf H})\,d\Omega\right) \over \int \vec{\bf H}^{\ast} \cdot \mathhat{\mu}\vec{\bf H}\,d\Omega}\eqno{\hbox{(1)}}$$ where Formula$\vec{\bf H}$ is the full-vectorial complex magnetic field; Formula$\mathhat{\varepsilon}$ and Formula$\mathhat{\mu}$ are the permittivity and permeability, respectively, of the waveguide; Formula$\varepsilon_{0}$ is the permittivity of the free space; Formula$\omega^{2}$ is the eigenvalue, where Formula$\omega$ is the angular frequency of the wave; and Formula$\alpha$ is a dimensionless parameter used to impose the divergence-free condition of the magnetic field in a least squares sense. In this formulation, both the Formula$\mathhat{\varepsilon}$ and Formula$\mathhat{\mu}$ parameters can be arbitrary complex tensors with possible off-diagonal coefficients, suitable to characterize electrooptic, acoustooptic, and elastooptic devices.

Finally, to analyze the coupling between a PCF and an optical fiber, the overlap integral method can be used to find the transmission coefficients and a simpler impedance-based approach can be used to find the reflection coefficients at the junction interfaces. However, it has been shown that the LSBR method [19], [27] is rigorously convergent and it also can be used to obtain both the transmission and reflection coefficients by considering all the guided and discretized radiation modes of the structures. This LSBR method has been used here to find the power coupling between a butt-coupled PCF and conventional optical fibers. On the other hand, a versatile FDTD [33] approach can also be used to study scattering coefficients at a junction, but this approach is numerically very expensive.



2.1. Analysis of an SMF

In this paper, the MFA is studied in some detail; however it is important to note that there have been various alternative definitions to represent this particular parameter. The MFA can be represented by the spot-size Formula$\sigma$, the effective area Formula$A_{\rm eff}$, and the Area second moment of intensity Formula$A_{\rm SMI}$. The spot-size is usually defined as the area where the field intensity falls to Formula$1/e$ of its maximum value (or where power intensity is Formula$1/e^{2}$) [18], [19]. The effective area Formula$A_{\rm eff} = ((\int\vert E\vert^{2})dA)^{2}/(\int\vert E\vert^{4}dA))$, where Formula$E$ is the electric field amplitude [29]. The Area second moment of the optical intensity Formula$A_{\rm SMI} = 2\surd((\int x^{2}I(x, y)/(\int I(x, y)))$, where Formula$I(x, y)$ is the second moment of the intensity distribution profile [30]. Initially, a simple circular fiber is considered to study its MFA. The refractive indices of the silica cladding and the Ge-doped core are taken as 1.445 and 1.4502, respectively, at the operating wavelength of 1.55 Formula$\mu\hbox{m}$. Since, the TE and TM modes are degenerate; only the quasi-TM mode (with the dominant Formula$H^{x}$ and Formula$E^{y}$ fields) is considered in this analysis.

The variations of the effective index and the different MFAs with the core radius for this optical fiber are shown in Fig. 1. The effective index is defined as Formula$n_{e} = \beta/k_{o}$, where Formula$\beta$ is the propagation constant and the wavenumber Formula$k_{o} = 2 \pi/\lambda$. It is shown that as the core radius is reduced, the effective index is monotonically reduced. Several MFA designs were studied carefully for different core radii. As the core radius is reduced, initially the MFAs reduce but as cutoff region approaches, the MFAs begin to increase again. However, their values and expansion regimes are slightly different. The values for these MFAs were slightly different but they become identical at Formula$R = 5.0\ \mu\hbox{m}$. An SMF often has a radius of between 4.5 and 5.0 Formula$\mu\hbox{m}$. A closer investigation has revealed that the field profile at Formula$R = 5.0\ \mu\hbox{m}$ closely follows a Gaussian profile, which suggests that for a Gaussian shaped field profile, all the different MFA definitions may lead to a similar value. However, when the radius was larger than 5.0 Formula$\mu\hbox{m}$, it was observed that in the field decay rate in the cladding was faster than its equivalent Gaussian profile suggests. Similarly, for a radius smaller than 5.0 Formula$\mu\hbox{m}$, the field decays slowly in the cladding region compared with its equivalent Gaussian fitting profile. Thus, an MFA defined by different approaches will likely have different values when the mode field is not Gaussian in shape.

Figure 1
Fig. 1. Variation of mode field area and effective index of an SMF against core radius Formula$R$.

2.2. Analysis of a Tapered PCF

In this section, the MFA of a PCF, the main subject of this research, is thoroughly investigated. The PCF considered here has a number of rings Formula$N$ (where in this case Formula$N = 7$), and its silica refractive index is taken as 1.445 at the operating wavelength of 1.55 Formula$\mu\hbox{m}$. The pitch Formula$\Lambda$ is varied from 2.0 to 0.4 Formula$\mu\hbox{m}$ with an air-hole diameter Formula$d = 0.4\Lambda$. Variations of the different MFA parameters with the pitch length Formula$\Lambda$ are shown in Fig. 2. The log scale is used for the MFA to cover the lower range more clearly. As the radius is reduced, the MFA initially reduces but then begins to increase again. It can be seen that all these parameters increase as the modal cutoff is approached; however, its spot-size Formula$\sigma$ also shows saturation. It should be noted that for a low-index contrast SMF, the modal field reduces monotonically in the cladding. However, due to the presence of air holes in a PCF, the field profile does not decay monotonically outside the core region. In the definition of the spot-size, only the localized field values are considered, whereas the Formula$A_{\rm eff}$ and Formula$A_{\rm SMI}$ use the integration of field profile, and these are more stable. Although these values give some indication of their MFAs and are useful to identify the size for optimum coupling, to calculate the coupling efficiency, the rigorous LSBR approach will be used.

Figure 2
Fig. 2. Variation of mode field areas of a PCF against the pitch Formula$\Lambda$.

The Formula$H_{x}$ field profile for the Formula$H_{11}^{x}$ mode is shown in Fig. 3 for a PCF with 7 air-hole rings, when Formula$\Lambda = 1.0\ \mu\hbox{m}$ and for all the rings Formula$d/\Lambda = 0.4$, and except for the last ring, where Formula$d_{7}/\Lambda = 0.8$. It can be observed that the field contours are not concentric circles but show “cheese-like” holes due to the presence of the air holes. The variation of the Formula$H_{x}$ along the Formula$x$-axis is also shown as an inset, clearly demonstrating the field variations are not monotonic, and the location field minima around the air holes are shown by arrows. Hence, the simple spot-size, which depends on the local field values, can be unreliable when used to describe the MFA of a PCF. Subsequently, to gauge the field expansion, the term Formula$A_{\rm eff}$ is used in this work.

Figure 3
Fig. 3. Formula$H_{x}$ field profile of the Formula$H_{11}^{x}$ mode for Formula$N = 7$, Formula$\Lambda = 1.0$, Formula$d/\Lambda = 0.4$, and Formula$d_{7}/\Lambda = 0.8$.

Variations of the effective areas Formula$A_{\rm eff}$ with the pitch for a PCF with 5 air-hole rings are shown in Fig. 4. Here, the effect of the field expansion for two different air-hole ratios Formula$d/\Lambda$ are shown, besides the effect of having a larger air hole in the last ring (which also is shown). When all the air holes are of identical diameter and either Formula$0.4\Lambda$ or Formula$0.5\Lambda$, the value of Formula$A_{\rm eff}$ increases exponentially as Formula$\Lambda$ is reduced. It can be observed that for a smaller Formula$d/\Lambda = 0.4$, the effective area Formula$A_{\rm eff}$ becomes higher due to the smaller size of the air holes, compared with that where Formula$d/\Lambda = 0.5$. It can also be observed that as larger air holes were introduced in the outermost ring (5th ring, shown as an inset), the value of the MFA is forced to remain flatter than it would have been otherwise at lower values of pitch. In the case of Formula$d/\Lambda = 0.4$, all the air holes in the first four rings have their dimension Formula$d = 0.4\Lambda$ except the fifth ring which has a larger dimension, which denoted by Formula$d_{5} = 0.8\Lambda$. This ensures that the MFA is stable at the lower pitch values without it expanding exponentially and the mode expansion slows down by the last ring, which has larger air holes. This would allow stable coupling to occur without much error or uncertainty even if there were structural variations occurring during the fabrication or tapering. This figure also demonstrates that a PCF with smaller air holes in most of the inner rings and larger air holes in the last ring is expected to produce a larger Formula$A_{\rm eff}$, which is also reasonably stable with the pitch variation. There are also some random variations which occur due to mode degeneration with the cladding modes [31].

Figure 4
Fig. 4. Variations of the Formula$A_{\rm eff}$ with the pitch length for PCF having Formula$d/\Lambda = 0.4\ \hbox{and}\ 0.5$ for Formula$N = 5$.

Next, the variations of the effective areas Formula$A_{\rm eff}$ with the pitch are shown in Fig. 5 for two different numbers of air-hole rings, given by Formula$N = 5\ \hbox{and}\ 7$. In both cases, Formula$d/\Lambda$ is taken as 0.4, and additional curves are also shown when the air-hole diameter in the last ring is increased to Formula$0.8\Lambda$. It can be noted that when all the air-hole diameters are of the same size for all the rings, the value of Formula$A_{\rm eff}$ increases progressively as the pitch Formula$\Lambda$ is reduced. When the number of rings is large, the value of Formula$A_{\rm eff}$ is slightly larger as there is a larger cladding region available into which the mode can expand. It is also shown in Fig. 5 that by using 7 rings Formula$(N = 7)$ and having the same diameter air holes in the last ring (seventh), a higher Formula$A_{\rm eff}$ value can be obtained, but this would be very sensitive to the pitch value. However, as the air-hole diameter of the last ring is increased, in both cases, the value of Formula$A_{\rm eff}$ stabilizes. It can be also noted here that this Formula$A_{\rm eff}$ value is stable when the air-hole diameter in the last ring is large, where Formula$d = 0.8\Lambda$ and with a smaller value of the pitch, Formula$A_{\rm eff}$ shows a lower variation with the pitch. This suggests that if the terminal dimension of a tapered PCF is taken as Formula$\Lambda = 0.7\ \mu\hbox{m}$, a smaller variation of pitch due to the fabrication tolerances would not change Formula$A_{\rm eff}$ significantly. For Formula$N = 7$, when all the air holes in the first six rings have a dimension Formula$d = 0.4\Lambda$ (except the air holes in the 7th ring with the dimension of Formula$d_{7} = 0.8\Lambda$), the stabilized value of MFA is around 20 Formula$\mu\hbox{m}^{2}$.

Figure 5
Fig. 5. Variations of the Formula$A_{\rm eff}$ with the pitch length for PCF having Formula${\rm d}/\Lambda = 0.4$ for Formula${\rm N} = 5$ and Formula${\rm N} = 7$.

As can be observed, when the number of rings in the cladding, N, is increased, this results in an increase in the MFA as well. This shows that with a higher number of rings it is possible to achieve a very high MFA that is comparable with that of SMF or if needed to be comparable to that of an erbium-doped fiber amplifier (EDFA); this would then result in a lowering of the insertion loss when butt-coupled to these fibers.

2.3. Coupling Between PCF and Optical Fiber

Finally, the Coupling Efficiency is calculated rigorously by using the LSBR method [27]. In Fig. 5, it was shown that a stable value of Formula$A_{\rm eff} = 20\ \mu\hbox{m}$ can be obtained for Formula$N = 7$ with all the air-hole diameters Formula$d = 0.4\Lambda$, except that of the last ring, where Formula$d_{7} = 0.8\Lambda$. A typical EDFA may have an Formula$A_{\rm eff}$ value around 25 Formula$\mu\hbox{m}^{2}$ and an SMF have its Formula$A_{\rm eff}$ around 80 Formula$\mu\hbox{m}^{2}$. Thus a tapered PCF with Formula$N = 7$, Formula$d/\Lambda = 0.4$ and a final (seventh) hole ratio Formula$d_{7}/\Lambda = 0.8\ \mu \hbox{m}$, as shown above, could be efficiently coupled to an EDFA or a lensed fiber with a similar MFA.

The variations of the Coupling Efficiency with the pitch length for a PCF with 7 rings are shown in Fig. 6 when it is butt-coupled to an EDFA. In this case the core and cladding indices of the EDFA are taken to be 1.46178 and 1.445, respectively and its radius is taken as 2.5 Formula$\mu\hbox{m}$. When all the air holes are equal to Formula$0.4\Lambda$, the Coupling Efficiency to this EDFA is shown by a dashed line and when the diameters of the air holes in the last ring are increased to Formula$0.8\Lambda$, this is shown by a solid line. A log-scale is used for the coupling efficiency to show the lower value more clearly.

Figure 6
Fig. 6. Variations of the coupled power to an EDFA with the tapered pitch Formula$\Lambda$ of a PCF.

It can be observed that with the outer rings having larger air holes, as the pitch length is reduced from 2.0 to 0.5 Formula$\mu\hbox{m}$, the coupled power is seen to be stable over the range of lower values of pitch (for Formula$\Lambda = 0.7$Formula$1.0\ \mu\hbox{m}$), as shown by the solid line. In this case, the value of the MFA of the PCF has an expanded, as well as a stable value, as shown earlier in Fig. 5, yielding a very stable power Coupling Efficiency with its maximum value of Formula$\sim$0.95, which can be achieved at Formula$\Lambda = 0.85\ \mu\hbox{m}$.

However, the power coupling to an EDFA, for a PCF with all the air holes identical (dashed line), not only shows a lower Coupling Efficiency but also shows a random variation in the coupling coefficient. This is due to the degeneration of the core mode with the cladding mode which is particularly frequent near cutoff. Previously, it had been reported that a PCF near cutoff or when bent shows that the loss value is erratic due to mode degeneration [31], [32] of the core mode with the surface modes in the extensive solid outer cladding. Similarly, it has been observed here that the presence of a larger air hole reduces the silica area near the boundary and consequently reduces the possibility mode degeneration, resulting in a more stable in the coupling efficiency. Hence, it is shown that by increasing the diameter of the last air-hole ring, the expanded modes are more isolated from the high index outer cladding region and mode degeneration is also avoided. Thus a stable coupling can be achieved over a range of the pitch lengths which is stable during the possible change of the pitch when the PCF is tapered. Such an approach would also be more tolerant against waveguides misalignment, as the spot-sizes are being expanded in this case.

Next, the number of rings is increased to study the degree to which expansion of spot-size which can be achieved. The variation of the effective area Formula$A_{\rm eff}$ with the reduction of the pitch Formula$\Lambda$ is shown in Fig. 7 for Formula$N = 7, 8,\ \hbox{and}\ 10$. In all the cases, the air-hole diameter of the last ring has been increased to Formula$0.8\Lambda$ to stabilize the MFA near their cutoff conditions.

Figure 7
Fig. 7. Variations of the Formula$A_{\rm eff}$ with the pitch length for PCFs having Formula$d/\Lambda = 0.4$ and outermost Formula$d/\Lambda = 0.8$ for Formula$N = 7, 8,\ \hbox{and}\ 10$.

In each case as the pitch is reduced, the MFA increases as the PCF designs approaches their cutoff, but due to the presence of larger air holes in all the cases the MFA reaches a maximum value. However, it can be observed that for higher ring numbers, the maximum Formula$A_{\rm eff}$ value was higher, which would allow efficient coupling to an optical fiber with a large MFA.

From the work done, it is clear that different numbers of rings are best suited for coupling of a PCF to an SMF, EDFA or lensed fiber. Next, the mode shape area required from the different optical fibers, all of which guide a single moded waveguide, is studied by adjusting the radius and index contrast to maintain them identical. In this case, the cladding refractive index is taken as 1.445, and the core index is adjusted for each fiber diameter to have the same normalized dimension Formula$V$.

The variation of the required refractive index of the core with its radius Formula$a$ is shown in Fig. 8, designed to maintain the single modedness by keeping the V parameter fixed at Formula$V = 2.23821417$, which is that of a typical SMF. The variation of the MFA, Formula$A_{\rm eff}$ with the radius for this fiber with a constant value of Formula$V$ (where Formula$V = 2.23821417$) is also shown here. It can be observed that as Formula$a$ is reduced, the value of Formula$A_{\rm eff}$ also reduces.

Figure 8
Fig. 8. Variation of Formula$A_{\rm eff}$ and core refractive index difference Formula$n_{g}$ of an SMF against fiber radius Formula$a$.

Next, the butt-coupling between a tapered PCF with Formula$N = 8$ to an optical fiber with Formula$a = 3.5\ \mu\hbox{m} (V = 2.23821417)$ is studied. The variation of the coupling efficiency of a PCF with Formula$N = 8$ to an optical fiber with Formula$a = 3.5\ \mu\hbox{m}$ with the final pitch length Formula$\Lambda$ is shown in Fig. 9 for both equal air holes and larger air holes in the last ring (eight) by a dashed and a solid line, respectively.

Figure 9
Fig. 9. Variation of Coupling Efficiency to PCF with tapered pitch Formula$\Lambda$ and SMF Formula$a = 3.5\ \mu\hbox{m}$.

It is shown here that the maximum coupling efficiency (of 95%) can be achieved when the pitch length was 0.85 Formula$\mu\hbox{m}$ and butt-coupled to this fiber with Formula$a = 3.5\ \mu\hbox{m}$. During the tapering process, if the pitch value change between 0.7 Formula$\mu\hbox{m}$ to 1.0 Formula$\mu\hbox{m}$, the coupling efficiency will still be above 90%. This shows the design is very stable, with the possible adjustment of the terminating pitch length for a tapered PCF. However, using the design principle discussed, for coupling to an SMF, Formula$A_{\rm eff}$ needs to be further increased to a value close to that of an SMF. As the number of rings is further increased, the expansion of the mode field profiles closer to cutoff increases as well, hence, allowing for more effective coupling to an SMF.

Therefore, it can be seen that when a PCF is down-tapered for coupling, the variations in the dimensions of the pitch or the diameter of the air holes that may arise as result of the fabrication or tapering process would not affect appreciably the power coupled between a PCF and an SMF or an EDFA.



A novel design approach for a PCF which could be considered as a candidate for efficient coupling to an optical fiber has been presented. Initially various MFA parameters and field profiles for an SMF and a PCF were studied. It has been shown here that a smaller air-hole diameter and a larger number of rings would allow the Formula$A_{\rm eff}$ value to reach a higher value, which can be achieved by operating a PCF near cutoff. However, as its expansion near cutoff can be very rapid and unstable, by increasing the air-hole diameter in the last ring, this parameter can be stabilized with the variation of the fabrication tolerances. Using this approach presented above, it is possible to avoid uncertainty resulting from the variations in the dimensions of the pitch or the diameters of the air holes in the PCF as a result of fabrication or tapering, thereby ensuring that the PCF can be successfully coupled to an optical fiber without any significant loss in coupled power. Additionally, it is also shown here that the largest air holes in the last ring reduce the mode degeneration with the cladding modes. During the tapering process it has been assumed that the pitch Formula$\Lambda$ reduces gradually while keeping the Formula$d/\Lambda$ ratio constant. However, the air holes can also collapse, and the air-hole/pitch ratio can also change, although this may give an additional flexibility, as well as an additional parameter to optimize the situation. Once the nature of the deviations are known a priori then a rigorous numerical approach, such as that presented above, can be used to optimize the designs before their fabrication for experimental use. In this approach, as the PCF operates near cutoff, it is normally expected that the leakage and bending losses will be increased. However, in this approach, since larger hole diameters are used in the last air-hole ring, in fact, rather, lower leakage and bending losses are expected. Additionally, if required additional air-hole rings with larger hole diameters can be included and the design can be optimized [34] to reduce leakage and bending losses further.


Corresponding author: M. Uthman (e-mail:


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M. Uthman

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B. M. A. Rahman

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N. Kejalakshmy

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A. Agrawal

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H. Abana

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K. T. V. Grattan

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