An Effective AUSM-Type Scheme for Both Cases of Low Mach Number and High Mach Number

A new scheme called AUSMAS (Advection Upstream Splitting Method for All Speeds) is proposed for both high speed and low speed simulation cases. For the cases of low speed, it controls the checkerboard decoupling by keeping the coefficient of the pressure difference to the order of O(Ma<sup<−1&...
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Autor*in:	Nan Li [verfasserIn] Feng Qu [verfasserIn] Di Sun [verfasserIn] Guanghui Wu [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2022

Schlagwörter:	shock anomaly AUSM all speeds AUSMAS computational fluid dynamics

Übergeordnetes Werk:	In: Applied Sciences - MDPI AG, 2012, 12(2022), 11, p 5464
Übergeordnetes Werk:	volume:12 ; year:2022 ; number:11, p 5464

Links:	Link aufrufen Link aufrufen Link aufrufen Journal toc

DOI / URN:	10.3390/app12115464

Katalog-ID:	DOAJ021334633

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520			\|a A new scheme called AUSMAS (Advection Upstream Splitting Method for All Speeds) is proposed for both high speed and low speed simulation cases. For the cases of low speed, it controls the checkerboard decoupling by keeping the coefficient of the pressure difference to the order of O(Ma<sup<−1</sup<) in the mass flux. Furthermore, it is able to guarantee a high level of accuracy by keeping the coefficients of the dissipation terms to the order of O(Ma<sup<0</sup<) in the momentum flux. For the cases of high speeds, especially at supersonic and hypersonic speeds, it is able to avoid the appearance of the shock anomaly by controlling the coefficients of the density perturbation in the mass flux. AUSMAS is testified to have the following attractive properties according to various numerical tests: (1) robustness against the abnormal shock; (2) high resolution in discontinuity; (3) the appearance of the unphysical expansion shock is avoided; (4) high resolution and low dissipation at low speeds; (5) independent of any tuning coefficient. These properties determined that AUSMAS has great promise in efficiently and accurately simulating flows of all speeds.
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language	English
source	In Applied Sciences 12(2022), 11, p 5464 volume:12 year:2022 number:11, p 5464
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topic_facet	shock anomaly AUSM all speeds AUSMAS computational fluid dynamics Technology T Engineering (General). Civil engineering (General) Biology (General) Physics Chemistry
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container_title	Applied Sciences
authorswithroles_txt_mv	Nan Li @@aut@@ Feng Qu @@aut@@ Di Sun @@aut@@ Guanghui Wu @@aut@@
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callnumber-first	T - Technology
author	Nan Li
spellingShingle	Nan Li misc TA1-2040 misc QH301-705.5 misc QC1-999 misc QD1-999 misc shock anomaly misc AUSM misc all speeds misc AUSMAS misc computational fluid dynamics misc Technology misc T misc Engineering (General). Civil engineering (General) misc Biology (General) misc Physics misc Chemistry An Effective AUSM-Type Scheme for Both Cases of Low Mach Number and High Mach Number
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topic_title	TA1-2040 QH301-705.5 QC1-999 QD1-999 An Effective AUSM-Type Scheme for Both Cases of Low Mach Number and High Mach Number shock anomaly AUSM all speeds AUSMAS computational fluid dynamics
topic	misc TA1-2040 misc QH301-705.5 misc QC1-999 misc QD1-999 misc shock anomaly misc AUSM misc all speeds misc AUSMAS misc computational fluid dynamics misc Technology misc T misc Engineering (General). Civil engineering (General) misc Biology (General) misc Physics misc Chemistry
topic_unstemmed	misc TA1-2040 misc QH301-705.5 misc QC1-999 misc QD1-999 misc shock anomaly misc AUSM misc all speeds misc AUSMAS misc computational fluid dynamics misc Technology misc T misc Engineering (General). Civil engineering (General) misc Biology (General) misc Physics misc Chemistry
topic_browse	misc TA1-2040 misc QH301-705.5 misc QC1-999 misc QD1-999 misc shock anomaly misc AUSM misc all speeds misc AUSMAS misc computational fluid dynamics misc Technology misc T misc Engineering (General). Civil engineering (General) misc Biology (General) misc Physics misc Chemistry
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title	An Effective AUSM-Type Scheme for Both Cases of Low Mach Number and High Mach Number
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title_full	An Effective AUSM-Type Scheme for Both Cases of Low Mach Number and High Mach Number
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title_sort	effective ausm-type scheme for both cases of low mach number and high mach number
callnumber	TA1-2040
title_auth	An Effective AUSM-Type Scheme for Both Cases of Low Mach Number and High Mach Number
abstract	A new scheme called AUSMAS (Advection Upstream Splitting Method for All Speeds) is proposed for both high speed and low speed simulation cases. For the cases of low speed, it controls the checkerboard decoupling by keeping the coefficient of the pressure difference to the order of O(Ma<sup<−1</sup<) in the mass flux. Furthermore, it is able to guarantee a high level of accuracy by keeping the coefficients of the dissipation terms to the order of O(Ma<sup<0</sup<) in the momentum flux. For the cases of high speeds, especially at supersonic and hypersonic speeds, it is able to avoid the appearance of the shock anomaly by controlling the coefficients of the density perturbation in the mass flux. AUSMAS is testified to have the following attractive properties according to various numerical tests: (1) robustness against the abnormal shock; (2) high resolution in discontinuity; (3) the appearance of the unphysical expansion shock is avoided; (4) high resolution and low dissipation at low speeds; (5) independent of any tuning coefficient. These properties determined that AUSMAS has great promise in efficiently and accurately simulating flows of all speeds.
abstractGer	A new scheme called AUSMAS (Advection Upstream Splitting Method for All Speeds) is proposed for both high speed and low speed simulation cases. For the cases of low speed, it controls the checkerboard decoupling by keeping the coefficient of the pressure difference to the order of O(Ma<sup<−1</sup<) in the mass flux. Furthermore, it is able to guarantee a high level of accuracy by keeping the coefficients of the dissipation terms to the order of O(Ma<sup<0</sup<) in the momentum flux. For the cases of high speeds, especially at supersonic and hypersonic speeds, it is able to avoid the appearance of the shock anomaly by controlling the coefficients of the density perturbation in the mass flux. AUSMAS is testified to have the following attractive properties according to various numerical tests: (1) robustness against the abnormal shock; (2) high resolution in discontinuity; (3) the appearance of the unphysical expansion shock is avoided; (4) high resolution and low dissipation at low speeds; (5) independent of any tuning coefficient. These properties determined that AUSMAS has great promise in efficiently and accurately simulating flows of all speeds.
abstract_unstemmed	A new scheme called AUSMAS (Advection Upstream Splitting Method for All Speeds) is proposed for both high speed and low speed simulation cases. For the cases of low speed, it controls the checkerboard decoupling by keeping the coefficient of the pressure difference to the order of O(Ma<sup<−1</sup<) in the mass flux. Furthermore, it is able to guarantee a high level of accuracy by keeping the coefficients of the dissipation terms to the order of O(Ma<sup<0</sup<) in the momentum flux. For the cases of high speeds, especially at supersonic and hypersonic speeds, it is able to avoid the appearance of the shock anomaly by controlling the coefficients of the density perturbation in the mass flux. AUSMAS is testified to have the following attractive properties according to various numerical tests: (1) robustness against the abnormal shock; (2) high resolution in discontinuity; (3) the appearance of the unphysical expansion shock is avoided; (4) high resolution and low dissipation at low speeds; (5) independent of any tuning coefficient. These properties determined that AUSMAS has great promise in efficiently and accurately simulating flows of all speeds.
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title_short	An Effective AUSM-Type Scheme for Both Cases of Low Mach Number and High Mach Number
url	https://doi.org/10.3390/app12115464 https://doaj.org/article/2aa856773a66444789afd11827d633ea https://www.mdpi.com/2076-3417/12/11/5464 https://doaj.org/toc/2076-3417
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An Effective AUSM-Type Scheme for Both Cases of Low Mach Number and High Mach Number

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