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multiphysics finite element physical modeling program  (COMSOL Inc)

 
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    COMSOL Inc multiphysics finite element physical modeling program
    ( A , C , and E ) The geometries and boundary conditions of COMSOL <t>Multiphysics</t> finite element thermal models for schematic cross sections of the crust and upper mantle in the region of the CE5 landing site. Compositions and thermal conductivities used for all models are shown in (A) and discussed in Materials and Methods. The upper KREEP layer represents Imbrium ejecta to the east of the CE5 landing site and begins generating heat at 3.9 Ga in all models. The lower KREEP layer has the composition of high-K KREEP . See Materials and Methods for more details on initial model conditions. ( B , D , and F ) Model results showing the temperature profiles of the crust and upper mantle at 2 Ga for each model. As these models are purely conductive and absolute temperatures are not necessarily applicable to the mantle, but rather these models show the relative heating effects of a subcrustal KREEP layer of either 5 km (D) or 10 km (F) thickness.
    Multiphysics Finite Element Physical Modeling Program, supplied by COMSOL 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/multiphysics+model/pmc12273790-232-35-34?v=COMSOL+Inc
    Average 90 stars, based on 1 article reviews
    multiphysics finite element physical modeling program - by Bioz Stars, 2026-08
    90/100 stars

    Images

    1) Product Images from "A shallow mantle source for the Chang’e 5 lavas reveals how top-down heating prolonged lunar magmatism"

    Article Title: A shallow mantle source for the Chang’e 5 lavas reveals how top-down heating prolonged lunar magmatism

    Journal: Science Advances

    doi: 10.1126/sciadv.adr1486

    ( A , C , and E ) The geometries and boundary conditions of COMSOL Multiphysics finite element thermal models for schematic cross sections of the crust and upper mantle in the region of the CE5 landing site. Compositions and thermal conductivities used for all models are shown in (A) and discussed in Materials and Methods. The upper KREEP layer represents Imbrium ejecta to the east of the CE5 landing site and begins generating heat at 3.9 Ga in all models. The lower KREEP layer has the composition of high-K KREEP . See Materials and Methods for more details on initial model conditions. ( B , D , and F ) Model results showing the temperature profiles of the crust and upper mantle at 2 Ga for each model. As these models are purely conductive and absolute temperatures are not necessarily applicable to the mantle, but rather these models show the relative heating effects of a subcrustal KREEP layer of either 5 km (D) or 10 km (F) thickness.
    Figure Legend Snippet: ( A , C , and E ) The geometries and boundary conditions of COMSOL Multiphysics finite element thermal models for schematic cross sections of the crust and upper mantle in the region of the CE5 landing site. Compositions and thermal conductivities used for all models are shown in (A) and discussed in Materials and Methods. The upper KREEP layer represents Imbrium ejecta to the east of the CE5 landing site and begins generating heat at 3.9 Ga in all models. The lower KREEP layer has the composition of high-K KREEP . See Materials and Methods for more details on initial model conditions. ( B , D , and F ) Model results showing the temperature profiles of the crust and upper mantle at 2 Ga for each model. As these models are purely conductive and absolute temperatures are not necessarily applicable to the mantle, but rather these models show the relative heating effects of a subcrustal KREEP layer of either 5 km (D) or 10 km (F) thickness.

    Techniques Used:



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    (a) The output power measured experimentally for TEC cells with different electrode separation ( i.e. electrolyte or hydrogel thickness) as a function of voltage. (b) V oc and current density calculated with a complete COMSOL <t>multiphysics</t> simulation as a function of electrode separation. (c) The experimental result for the maximum output power as a function of electrode separation along with a 3rd-order polynomial fit just to underline the trend. (d) The convection velocity at the electrode/electrolyte interface obtained for cells with 10 mm width and different heights, explaining the reason for the performance decay after 20 mm (obtained from simulations).
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    Image Search Results


    ( A , C , and E ) The geometries and boundary conditions of COMSOL Multiphysics finite element thermal models for schematic cross sections of the crust and upper mantle in the region of the CE5 landing site. Compositions and thermal conductivities used for all models are shown in (A) and discussed in Materials and Methods. The upper KREEP layer represents Imbrium ejecta to the east of the CE5 landing site and begins generating heat at 3.9 Ga in all models. The lower KREEP layer has the composition of high-K KREEP . See Materials and Methods for more details on initial model conditions. ( B , D , and F ) Model results showing the temperature profiles of the crust and upper mantle at 2 Ga for each model. As these models are purely conductive and absolute temperatures are not necessarily applicable to the mantle, but rather these models show the relative heating effects of a subcrustal KREEP layer of either 5 km (D) or 10 km (F) thickness.

    Journal: Science Advances

    Article Title: A shallow mantle source for the Chang’e 5 lavas reveals how top-down heating prolonged lunar magmatism

    doi: 10.1126/sciadv.adr1486

    Figure Lengend Snippet: ( A , C , and E ) The geometries and boundary conditions of COMSOL Multiphysics finite element thermal models for schematic cross sections of the crust and upper mantle in the region of the CE5 landing site. Compositions and thermal conductivities used for all models are shown in (A) and discussed in Materials and Methods. The upper KREEP layer represents Imbrium ejecta to the east of the CE5 landing site and begins generating heat at 3.9 Ga in all models. The lower KREEP layer has the composition of high-K KREEP . See Materials and Methods for more details on initial model conditions. ( B , D , and F ) Model results showing the temperature profiles of the crust and upper mantle at 2 Ga for each model. As these models are purely conductive and absolute temperatures are not necessarily applicable to the mantle, but rather these models show the relative heating effects of a subcrustal KREEP layer of either 5 km (D) or 10 km (F) thickness.

    Article Snippet: A series of two-dimensional thermal evolution models for a simplified east-west cross section of the local region of the Moon in northern Oceanus Procellarum where the CE5 basalts were collected were constructed using the COMSOL Multiphysics finite element physical modeling program.

    Techniques:

    (a) The output power measured experimentally for TEC cells with different electrode separation ( i.e. electrolyte or hydrogel thickness) as a function of voltage. (b) V oc and current density calculated with a complete COMSOL multiphysics simulation as a function of electrode separation. (c) The experimental result for the maximum output power as a function of electrode separation along with a 3rd-order polynomial fit just to underline the trend. (d) The convection velocity at the electrode/electrolyte interface obtained for cells with 10 mm width and different heights, explaining the reason for the performance decay after 20 mm (obtained from simulations).

    Journal: Materials Horizons

    Article Title: Hydrogel-based thermoelectrochemical cells for waste heat recovery under passive cooling conditions

    doi: 10.1039/d5mh00771b

    Figure Lengend Snippet: (a) The output power measured experimentally for TEC cells with different electrode separation ( i.e. electrolyte or hydrogel thickness) as a function of voltage. (b) V oc and current density calculated with a complete COMSOL multiphysics simulation as a function of electrode separation. (c) The experimental result for the maximum output power as a function of electrode separation along with a 3rd-order polynomial fit just to underline the trend. (d) The convection velocity at the electrode/electrolyte interface obtained for cells with 10 mm width and different heights, explaining the reason for the performance decay after 20 mm (obtained from simulations).

    Article Snippet: Using a comprehensive COMSOL Multiphysics model (Fig. S3 with parameters reported in Table S1, ESI ), we compare the thermal behavior of a conventional liquid electrolyte and a hydrogel-based electrolyte as a function of the electrode separations, while keeping the lateral dimensions of the cell constant (width W = 10 mm and depth D = 10 mm).

    Techniques: Convection