ROBUST GRID ADAPTATION FOR COMPLEX TRANSONIC FLOWS.

J. F. Dannenhoffer; J. R. Baron

ROBUST GRID ADAPTATION FOR COMPLEX TRANSONIC FLOWS.

Research output: Contribution to journal › Conference Article › peer-review

Abstract

This paper presents an adaptation method which has been developed for the computation of two-dimensional Euler flows. Irregularly shaped embedded regions, which are coupled to the base grid by a multiple-grid method, are employed to achieve any user-specified level of accuracy. The adaptation technique is applied to the computation of the AGARD Working Group 07 isolated airfoil test cases and an airfoil/flap combination.

Original language	English (US)
Journal	AIAA Paper
State	Published - 1986
Externally published	Yes

ASJC Scopus subject areas

General Engineering

Cite this

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title = "ROBUST GRID ADAPTATION FOR COMPLEX TRANSONIC FLOWS.",

abstract = "This paper presents an adaptation method which has been developed for the computation of two-dimensional Euler flows. Irregularly shaped embedded regions, which are coupled to the base grid by a multiple-grid method, are employed to achieve any user-specified level of accuracy. The adaptation technique is applied to the computation of the AGARD Working Group 07 isolated airfoil test cases and an airfoil/flap combination.",

author = "Dannenhoffer, {J. F.} and Baron, {J. R.}",

year = "1986",

language = "English (US)",

journal = "AIAA Paper",

issn = "0146-3705",

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T1 - ROBUST GRID ADAPTATION FOR COMPLEX TRANSONIC FLOWS.

AU - Dannenhoffer, J. F.

AU - Baron, J. R.

PY - 1986

Y1 - 1986

N2 - This paper presents an adaptation method which has been developed for the computation of two-dimensional Euler flows. Irregularly shaped embedded regions, which are coupled to the base grid by a multiple-grid method, are employed to achieve any user-specified level of accuracy. The adaptation technique is applied to the computation of the AGARD Working Group 07 isolated airfoil test cases and an airfoil/flap combination.

AB - This paper presents an adaptation method which has been developed for the computation of two-dimensional Euler flows. Irregularly shaped embedded regions, which are coupled to the base grid by a multiple-grid method, are employed to achieve any user-specified level of accuracy. The adaptation technique is applied to the computation of the AGARD Working Group 07 isolated airfoil test cases and an airfoil/flap combination.

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UR - http://www.scopus.com/inward/citedby.url?scp=0022564113&partnerID=8YFLogxK

M3 - Conference Article

AN - SCOPUS:0022564113

SN - 0146-3705

JO - AIAA Paper

JF - AIAA Paper

ER -

ROBUST GRID ADAPTATION FOR COMPLEX TRANSONIC FLOWS.

Abstract

ASJC Scopus subject areas

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