Accuracy recuitments for transient aerodynamics

Ken Mattsson; Magnus Svärd; Mark Carpenter; Jan Nordström

Accuracy recuitments for transient aerodynamics

Ken Mattsson, Magnus Svärd, Mark Carpenter, Jan Nordström

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

4 Citations (Scopus)

Abstract

A stable and high order accurate finite difference scheme is used to perform a numerical study on the benefit of high order methods. Numerical computations of a vortex-airfoil interaction governed by the Euler equations show that high order methods are required in order to capture the significant flow features for transient problems.

Original language	English
Title of host publication	16th AIAA Computational Fluid Dynamics Conference
Publication status	Published - 2003
Externally published	Yes
Event	16th AIAA Computational Fluid Dynamics Conference 2003 - Orlando, FL, United States Duration: 23 Jun 2003 → 26 Jun 2003

Publication series

Name	16th AIAA Computational Fluid Dynamics Conference

Conference

Conference	16th AIAA Computational Fluid Dynamics Conference 2003
Country/Territory	United States
City	Orlando, FL
Period	23/06/03 → 26/06/03

ASJC Scopus subject areas

Fluid Flow and Transfer Processes
Energy Engineering and Power Technology
Engineering (miscellaneous)
Aerospace Engineering
Automotive Engineering
Mechanical Engineering

Cite this

@inproceedings{68153d50cbdc428d9f89b3e4580067d3,

title = "Accuracy recuitments for transient aerodynamics",

abstract = "A stable and high order accurate finite difference scheme is used to perform a numerical study on the benefit of high order methods. Numerical computations of a vortex-airfoil interaction governed by the Euler equations show that high order methods are required in order to capture the significant flow features for transient problems.",

author = "Ken Mattsson and Magnus Sv{\"a}rd and Mark Carpenter and Jan Nordstr{\"o}m",

year = "2003",

language = "English",

isbn = "9781624100864",

series = "16th AIAA Computational Fluid Dynamics Conference",

booktitle = "16th AIAA Computational Fluid Dynamics Conference",

note = "16th AIAA Computational Fluid Dynamics Conference 2003 ; Conference date: 23-06-2003 Through 26-06-2003",

}

TY - GEN

T1 - Accuracy recuitments for transient aerodynamics

AU - Mattsson, Ken

AU - Svärd, Magnus

AU - Carpenter, Mark

AU - Nordström, Jan

PY - 2003

Y1 - 2003

N2 - A stable and high order accurate finite difference scheme is used to perform a numerical study on the benefit of high order methods. Numerical computations of a vortex-airfoil interaction governed by the Euler equations show that high order methods are required in order to capture the significant flow features for transient problems.

AB - A stable and high order accurate finite difference scheme is used to perform a numerical study on the benefit of high order methods. Numerical computations of a vortex-airfoil interaction governed by the Euler equations show that high order methods are required in order to capture the significant flow features for transient problems.

UR - http://www.scopus.com/inward/record.url?scp=84897584797&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84897584797

SN - 9781624100864

T3 - 16th AIAA Computational Fluid Dynamics Conference

BT - 16th AIAA Computational Fluid Dynamics Conference

T2 - 16th AIAA Computational Fluid Dynamics Conference 2003

Y2 - 23 June 2003 through 26 June 2003

ER -

Accuracy recuitments for transient aerodynamics

Abstract

Publication series

Conference

ASJC Scopus subject areas

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Cite this