Reliability of aerodynamic analysis using a moment method

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In this study, a reliability analysis was performed for the aerodynamic analysis. Among various reliability analysis methods, the moment method was used and the results were compared with other methods. The reliability of aerodynamic analysis of a 2D airfoil, a 3D wing and a wing body configuration were considered. In the case of 2D airfoil, the reliability was computed by parameterising an airfoil shape using the PARSEC function and considering uncertainties of its shape. In the case of 3D wing and wing body configuration, it was computed by considering uncertainties of flow conditions.
Publisher
TAYLOR FRANCIS LTD
Issue Date
2009
Language
English
Article Type
Article
Keywords

DESIGN OPTIMIZATION

Citation

INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS, v.23, no.6, pp.495 - 502

ISSN
1061-8562
DOI
10.1080/10618560902984422
URI
http://hdl.handle.net/10203/99364
Appears in Collection
AE-Journal Papers(저널논문)ME-Journal Papers(저널논문)
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