유선좌표계를 사용한 이차원 익형의 실속에 대한 부분포물형 Navier-Stokes 해석(Ⅰ) : 격자계 생성 및 층류동장 해석Analysis of Airfoil Stall Using Partially Parabolic Navier-Stokes Equations in Streamline Coordinates; Part I - Grid Generation and Laminar-Flow Analysis

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Using conformal mapping, several orthogonal curvilinear coordinates of 0-. H- and C-type are generated for an arbitary airfoil at incidence. The partially parabolic Navier-Stokes equations are solved for the laminar flow about an airfoil at incidence in the streamline coordinates. By comparing the result with that obtained in non-streamline but still orthogonal coordinates, it has been found that the present procedure is much more efficient and accurate. The equations written in this coordinate system are shown to be least prone to the numerical error.
Publisher
한국항공우주학회
Issue Date
1994
Language
English
Citation

한국항공우주학회지, v.22, no.2, pp.1 - 12

ISSN
1225-1348
URI
http://hdl.handle.net/10203/66017
Appears in Collection
ME-Journal Papers(저널논문)
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