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finite difference eigenmode simulations ansys lumerical  (ANSYS inc)

 
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    ANSYS inc finite difference eigenmode simulations ansys lumerical
    Finite Difference Eigenmode Simulations Ansys Lumerical, supplied by ANSYS inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
    https://www.bioz.com/product/eigenmode+solver/finite+difference+eigenmode++fde++solver/pmc11685101-141-12-16
    Average 90 stars, based on 1 article reviews
    finite difference eigenmode simulations ansys lumerical - by Bioz Stars, 2026-10
    90/100 stars

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    Article Title: Compact wideband and high gain horn slot antenna array fed by printed ridge gap waveguide for X band applications
    Article Snippet: The paper is organized as follows: First, the main design concept of the PRGW technology is discussed and the dispersion analysis using the Ansys HFSS eigen-mode solver is presented.

    Article Title: Avoiding lateral mode leakage in thin film lithium niobate waveguides for the generation of spectrally pure photons at telecom wavelengths
    Article Snippet: The simulations are performed using the finite difference eigenmode (FDE) solver in Ansys Lumerical software.

    Article Title: Edge-guided inverse design of digital metamaterials for ultra-high-capacity on-chip multi-dimensional interconnect
    Article Snippet: The nite-difference eigenmode (FDE) solver from ANSYS Lumerical is utilized to calculate the effective index of various orthogonal modes as a function of waveguide widths (see Fig. S2).

    Article Title: Sidelobe-Suppressed Silicon Waveguide Gratings Through Asymmetrically-Apodized Corrugations
    Article Snippet: We report detailed investigations on the impact of corrugation width design on the resulting sidelobe suppression from a Gaussian-apodized silicon waveguide gratings (SWGs).. To address the nonlinear relationship between the waveguide width and effective index, corrugation widths at inner and outer sidewalls of SWGs should be individually optimized to warrant a constant waveguide effective index mean along the light propagation, thus enables balanced Gaussian apodization for sidelobe suppression at both edges of optical stopband.. We also confirm that sidelobe-suppressed responses are reproducible from die-to-die and wafer-to-wafer despite of its rounded grating profile.

    Article Title: Edge-guided inverse design of digital metamaterial-based mode multiplexers for high-capacity multi-dimensional optical interconnect
    Article Snippet: The finite-difference eigenmode (FDE) solver from ANSYS Lumerical is utilized to calculate the effective index of various orthogonal modes as a function of waveguide widths (see Fig. S ).

    Article Title: Low-Loss and Power-Efficient Polarization-Diversity 4 × 4 Microring Switch on a Multi-Layer Si<sub>3</sub>N<sub>4</sub>-on-SOI Platform
    Article Snippet: Silicon optical switches show great potential in building the next generation of flexible switching nodes.. However, due to the birefringence nature of silicon waveguides, most of them are polarization sensitive, which significantly affects their practical applications.. Here, we demonstrate an integrated polarization-diversity crossbar optical switch on a multi-layer Si3N4-on-SOI platform, capable of handling random polarization states.

    Article Title: Efficient coupling between photonic waveguides and III-nitride quantum emitters in the UV-visible spectral range
    Article Snippet: In this study, we establish comprehensive design guidelines to maximize single-mode transmission by efficient coupling between a III-nitride quantum-dot-in-nanowire light emitter and a photonic waveguide in the ultraviolet-visible (UV-Vis) spectral range.. Considering feasible epitaxial growth, deposition, and fabrication techniques, this study performs detailed electromagnetic simulations to identify the design limits of viable material systems suitable for monolithic integration of vertical III-nitride nanowires on standard ridge waveguides.. We show that unlike systems operating in the near-infrared wavelengths, light coupling and transmission in the UV-Vis range are significantly constrained by substrate leakage and backreflection.

    Dispersion:

    Article Title: Time-bin entangled Bell state generation and tomography on thin-film lithium niobate
    Article Snippet: .. Optical circuits and delay lines are simulated using finite element (COMSOL Multiphysics), finite difference eigenmode simulations (Ansys Lumerical) and custom scripts to extract chromatic dispersion in the long spirals by taking into account anisotropy of the crystal (see ). ..



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    Schematic of the initial design of SBGW. ( a ) Top view of the Bragg grating. ( b ) Side view. The silicon slab height and width are 220 nm and 500 nm, respectively. The height, width ( \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${W}_{\mathrm{wing}}$$\end{document} ), and the thickness \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${T}_{\mathrm{wing}}$$\end{document} of the silicon wings are 220 nm, 220 nm and 150 nm, respectively. The air gap between the silicon waveguide and the wings is \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${W}_{\mathrm{air}}=40 \mathrm{nm}$$\end{document} , and the lattice constant \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\mathrm{a}$$\end{document} is 330 nm. ( c ) The band diagram with two hyperbolic band, simulated from the listed parameters by CST <t>eigenmode</t> solver. Orange and red circles indicate the proposed pump and signal frequencies, respectively.
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    Schematic of the initial design of SBGW. ( a ) Top view of the Bragg grating. ( b ) Side view. The silicon slab height and width are 220 nm and 500 nm, respectively. The height, width ( \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${W}_{\mathrm{wing}}$$\end{document} ), and the thickness \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${T}_{\mathrm{wing}}$$\end{document} of the silicon wings are 220 nm, 220 nm and 150 nm, respectively. The air gap between the silicon waveguide and the wings is \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${W}_{\mathrm{air}}=40 \mathrm{nm}$$\end{document} , and the lattice constant \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\mathrm{a}$$\end{document} is 330 nm. ( c ) The band diagram with two hyperbolic band, simulated from the listed parameters by CST eigenmode solver. Orange and red circles indicate the proposed pump and signal frequencies, respectively.

    Journal: Scientific Reports

    Article Title: Optical push broom effect by a moving refractive index front in a silicon Bragg waveguide

    doi: 10.1038/s41598-026-36302-x

    Figure Lengend Snippet: Schematic of the initial design of SBGW. ( a ) Top view of the Bragg grating. ( b ) Side view. The silicon slab height and width are 220 nm and 500 nm, respectively. The height, width ( \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${W}_{\mathrm{wing}}$$\end{document} ), and the thickness \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${T}_{\mathrm{wing}}$$\end{document} of the silicon wings are 220 nm, 220 nm and 150 nm, respectively. The air gap between the silicon waveguide and the wings is \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$${W}_{\mathrm{air}}=40 \mathrm{nm}$$\end{document} , and the lattice constant \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\mathrm{a}$$\end{document} is 330 nm. ( c ) The band diagram with two hyperbolic band, simulated from the listed parameters by CST eigenmode solver. Orange and red circles indicate the proposed pump and signal frequencies, respectively.

    Article Snippet: Figure c presents the simulated band diagram using the CST eigenmode solver.

    Techniques: