On the use of high order central difference schemes for differential equation based wall distance computations
A computationally efficient high-order solver is developed to compute the wall distances by solving the relevant partial differential equations, namely: Eikonal, Hamilton-Jacobi (HJ) and Poisson equations. In contrast to the upwind schemes widely used in the literature, we explore the suitability of...
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creator | Kakumani, Hemanth Chandra Vamsi Vadlamani, Nagabhushana Rao Tucker, Paul Gary |
description | A computationally efficient high-order solver is developed to compute the
wall distances by solving the relevant partial differential equations, namely:
Eikonal, Hamilton-Jacobi (HJ) and Poisson equations. In contrast to the upwind
schemes widely used in the literature, we explore the suitability of high-order
central difference schemes (explicit/compact) for the wall-distance
computation. While solving the Hamilton-Jacobi equation, the high-order central
difference schemes performed approximately $1.4-2.8$ times faster than the
upwind schemes with a marginal improvement in the solution accuracy. A new
pseudo HJ formulation based on the localized artificial diffusivity (LAD)
approach has been proposed. It is demonstrated to predict results with an
accuracy comparable to that of the Eikonal equation and the simulations are
$\approx$ 1.5 times faster than the baseline HJ solver using upwind schemes. A
curvature correction is also incorporated in the HJ equation to correct for the
near-wall errors due to concave/convex wall curvatures. We demonstrate the
efficacy of the proposed methods on both the steady and unsteady test cases and
exploit the unsteady wall-distance solver to estimate the instantaneous shape
and burning surface area of a dendrite propellant grain in a solid propellant
rocket motor. |
doi_str_mv | 10.48550/arxiv.2111.09859 |
format | Article |
fullrecord | <record><control><sourceid>arxiv_GOX</sourceid><recordid>TN_cdi_arxiv_primary_2111_09859</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2111_09859</sourcerecordid><originalsourceid>FETCH-LOGICAL-a679-543bb2b176a10698d9879a4ac001cf9eb3232d308e4031604706515bebdf8c943</originalsourceid><addsrcrecordid>eNo9j8tOxCAUhtm4MKMP4EpeoBUKtLA0E2_JJLOZfXOAg23SywjUy9trq3H1J_8t-Qi54ayUWil2B_Gzfy8rznnJjFbmkkzHieYO6ZKQzoF2_WtH5-gxUodTjjBQ34eAESeHNLkOR0w0zPHfzv1PB98WyP08UQsJPf2AYd2lDOvKzeN5yVuershFgCHh9Z_uyOnx4bR_Lg7Hp5f9_aGAujGFksLayvKmBs5qo73RjQEJjjHugkErKlF5wTRKJnjNZMNqxZVF64N2Rooduf293YDbc-xHiF_tCt5u4OIbNp1UiA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>On the use of high order central difference schemes for differential equation based wall distance computations</title><source>arXiv.org</source><creator>Kakumani, Hemanth Chandra Vamsi ; Vadlamani, Nagabhushana Rao ; Tucker, Paul Gary</creator><creatorcontrib>Kakumani, Hemanth Chandra Vamsi ; Vadlamani, Nagabhushana Rao ; Tucker, Paul Gary</creatorcontrib><description>A computationally efficient high-order solver is developed to compute the
wall distances by solving the relevant partial differential equations, namely:
Eikonal, Hamilton-Jacobi (HJ) and Poisson equations. In contrast to the upwind
schemes widely used in the literature, we explore the suitability of high-order
central difference schemes (explicit/compact) for the wall-distance
computation. While solving the Hamilton-Jacobi equation, the high-order central
difference schemes performed approximately $1.4-2.8$ times faster than the
upwind schemes with a marginal improvement in the solution accuracy. A new
pseudo HJ formulation based on the localized artificial diffusivity (LAD)
approach has been proposed. It is demonstrated to predict results with an
accuracy comparable to that of the Eikonal equation and the simulations are
$\approx$ 1.5 times faster than the baseline HJ solver using upwind schemes. A
curvature correction is also incorporated in the HJ equation to correct for the
near-wall errors due to concave/convex wall curvatures. We demonstrate the
efficacy of the proposed methods on both the steady and unsteady test cases and
exploit the unsteady wall-distance solver to estimate the instantaneous shape
and burning surface area of a dendrite propellant grain in a solid propellant
rocket motor.</description><identifier>DOI: 10.48550/arxiv.2111.09859</identifier><language>eng</language><subject>Computer Science - Computational Engineering, Finance, and Science ; Physics - Fluid Dynamics</subject><creationdate>2021-11</creationdate><rights>http://creativecommons.org/licenses/by/4.0</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>228,230,780,885</link.rule.ids><linktorsrc>$$Uhttps://arxiv.org/abs/2111.09859$$EView_record_in_Cornell_University$$FView_record_in_$$GCornell_University$$Hfree_for_read</linktorsrc><backlink>$$Uhttps://doi.org/10.48550/arXiv.2111.09859$$DView paper in arXiv$$Hfree_for_read</backlink></links><search><creatorcontrib>Kakumani, Hemanth Chandra Vamsi</creatorcontrib><creatorcontrib>Vadlamani, Nagabhushana Rao</creatorcontrib><creatorcontrib>Tucker, Paul Gary</creatorcontrib><title>On the use of high order central difference schemes for differential equation based wall distance computations</title><description>A computationally efficient high-order solver is developed to compute the
wall distances by solving the relevant partial differential equations, namely:
Eikonal, Hamilton-Jacobi (HJ) and Poisson equations. In contrast to the upwind
schemes widely used in the literature, we explore the suitability of high-order
central difference schemes (explicit/compact) for the wall-distance
computation. While solving the Hamilton-Jacobi equation, the high-order central
difference schemes performed approximately $1.4-2.8$ times faster than the
upwind schemes with a marginal improvement in the solution accuracy. A new
pseudo HJ formulation based on the localized artificial diffusivity (LAD)
approach has been proposed. It is demonstrated to predict results with an
accuracy comparable to that of the Eikonal equation and the simulations are
$\approx$ 1.5 times faster than the baseline HJ solver using upwind schemes. A
curvature correction is also incorporated in the HJ equation to correct for the
near-wall errors due to concave/convex wall curvatures. We demonstrate the
efficacy of the proposed methods on both the steady and unsteady test cases and
exploit the unsteady wall-distance solver to estimate the instantaneous shape
and burning surface area of a dendrite propellant grain in a solid propellant
rocket motor.</description><subject>Computer Science - Computational Engineering, Finance, and Science</subject><subject>Physics - Fluid Dynamics</subject><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><sourceid>GOX</sourceid><recordid>eNo9j8tOxCAUhtm4MKMP4EpeoBUKtLA0E2_JJLOZfXOAg23SywjUy9trq3H1J_8t-Qi54ayUWil2B_Gzfy8rznnJjFbmkkzHieYO6ZKQzoF2_WtH5-gxUodTjjBQ34eAESeHNLkOR0w0zPHfzv1PB98WyP08UQsJPf2AYd2lDOvKzeN5yVuershFgCHh9Z_uyOnx4bR_Lg7Hp5f9_aGAujGFksLayvKmBs5qo73RjQEJjjHugkErKlF5wTRKJnjNZMNqxZVF64N2Rooduf293YDbc-xHiF_tCt5u4OIbNp1UiA</recordid><startdate>20211108</startdate><enddate>20211108</enddate><creator>Kakumani, Hemanth Chandra Vamsi</creator><creator>Vadlamani, Nagabhushana Rao</creator><creator>Tucker, Paul Gary</creator><scope>AKY</scope><scope>GOX</scope></search><sort><creationdate>20211108</creationdate><title>On the use of high order central difference schemes for differential equation based wall distance computations</title><author>Kakumani, Hemanth Chandra Vamsi ; Vadlamani, Nagabhushana Rao ; Tucker, Paul Gary</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a679-543bb2b176a10698d9879a4ac001cf9eb3232d308e4031604706515bebdf8c943</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Computer Science - Computational Engineering, Finance, and Science</topic><topic>Physics - Fluid Dynamics</topic><toplevel>online_resources</toplevel><creatorcontrib>Kakumani, Hemanth Chandra Vamsi</creatorcontrib><creatorcontrib>Vadlamani, Nagabhushana Rao</creatorcontrib><creatorcontrib>Tucker, Paul Gary</creatorcontrib><collection>arXiv Computer Science</collection><collection>arXiv.org</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Kakumani, Hemanth Chandra Vamsi</au><au>Vadlamani, Nagabhushana Rao</au><au>Tucker, Paul Gary</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>On the use of high order central difference schemes for differential equation based wall distance computations</atitle><date>2021-11-08</date><risdate>2021</risdate><abstract>A computationally efficient high-order solver is developed to compute the
wall distances by solving the relevant partial differential equations, namely:
Eikonal, Hamilton-Jacobi (HJ) and Poisson equations. In contrast to the upwind
schemes widely used in the literature, we explore the suitability of high-order
central difference schemes (explicit/compact) for the wall-distance
computation. While solving the Hamilton-Jacobi equation, the high-order central
difference schemes performed approximately $1.4-2.8$ times faster than the
upwind schemes with a marginal improvement in the solution accuracy. A new
pseudo HJ formulation based on the localized artificial diffusivity (LAD)
approach has been proposed. It is demonstrated to predict results with an
accuracy comparable to that of the Eikonal equation and the simulations are
$\approx$ 1.5 times faster than the baseline HJ solver using upwind schemes. A
curvature correction is also incorporated in the HJ equation to correct for the
near-wall errors due to concave/convex wall curvatures. We demonstrate the
efficacy of the proposed methods on both the steady and unsteady test cases and
exploit the unsteady wall-distance solver to estimate the instantaneous shape
and burning surface area of a dendrite propellant grain in a solid propellant
rocket motor.</abstract><doi>10.48550/arxiv.2111.09859</doi><oa>free_for_read</oa></addata></record> |
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subjects | Computer Science - Computational Engineering, Finance, and Science Physics - Fluid Dynamics |
title | On the use of high order central difference schemes for differential equation based wall distance computations |
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