Fast and robust viscous/inviscid interaction code for wing flowfield calculations

Urpo J. Pesonen; Ramesh K. Agarwal; Seppo Laine

doi:10.2514/2.2660

Fast and robust viscous/inviscid interaction code for wing flowfield calculations

Urpo J. Pesonen
, Ramesh K. Agarwal
, Seppo Laine

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

3 Scopus citations

Abstract

In this study, a three-dimensional potential solution was combined with two-dimensional viscous/inviscid interaction flow analysis at several cross sections across the wing span. The resulting method provides a flow solution with the viscous effects taken into account.

Original language	English
Pages (from-to)	730-733
Number of pages	4
Journal	Unknown Journal
Volume	37
Issue number	4
DOIs	https://doi.org/10.2514/2.2660
State	Published - 2000

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title = "Fast and robust viscous/inviscid interaction code for wing flowfield calculations",

abstract = "In this study, a three-dimensional potential solution was combined with two-dimensional viscous/inviscid interaction flow analysis at several cross sections across the wing span. The resulting method provides a flow solution with the viscous effects taken into account.",

author = "Pesonen, \{Urpo J.\} and Agarwal, \{Ramesh K.\} and Seppo Laine",

year = "2000",

doi = "10.2514/2.2660",

language = "English",

volume = "37",

pages = "730--733",

journal = "Unknown Journal",

number = "4",

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TY - JOUR

T1 - Fast and robust viscous/inviscid interaction code for wing flowfield calculations

AU - Pesonen, Urpo J.

AU - Agarwal, Ramesh K.

AU - Laine, Seppo

PY - 2000

Y1 - 2000

N2 - In this study, a three-dimensional potential solution was combined with two-dimensional viscous/inviscid interaction flow analysis at several cross sections across the wing span. The resulting method provides a flow solution with the viscous effects taken into account.

AB - In this study, a three-dimensional potential solution was combined with two-dimensional viscous/inviscid interaction flow analysis at several cross sections across the wing span. The resulting method provides a flow solution with the viscous effects taken into account.

UR - https://www.scopus.com/pages/publications/0034226316

U2 - 10.2514/2.2660

DO - 10.2514/2.2660

M3 - Article

AN - SCOPUS:0034226316

VL - 37

SP - 730

EP - 733

JO - Unknown Journal

JF - Unknown Journal

IS - 4

ER -

Fast and robust viscous/inviscid interaction code for wing flowfield calculations

Abstract

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