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Computational Elements for High-fidelity Aerodynamic Analysis and Design Optimisation

Cited 3 time in Web of Science Cited 3 time in Scopus
Authors

Kim, Chongam

Issue Date
2010-11
Publisher
Defence Scientific Information & Documentation Centre
Citation
Defence Science Journal, Vol.60 No.6, pp.628-638
Abstract
The study reviews the role of computational fluid dynamics (CFD) in aerodynamic shape optimisation, and discusses some of the efficient design methodologies The article in the first part, numerical schemes required for high-fidelity aerodynamic flow analysis are discussed To accurately resolve high-speed flow physics, high-fidelity shock-stable schemes as well as intelligent limiting strategy mimicking multi-dimensional flow physics are essential Exploiting these numerical schemes, some applications for 3-D internal/external flow analyses were carried out with various grid systems which enable the treatment of complex geometries In the second part, depending on the number of design variables and the way to obtain sensitivities or design points, several global and local optimisation methods for aerodynamic shape optimisation are discussed To avoid the problem that solutions of gradient-based optimisation method, (GBOM) are often trapped in local optimum, remedy by combining GBOM with global optimum strategy, such as surrogate models and genetic algorithm (GA) has been examined As an efficient grid deformation tool grid deformation technique using NURBS function is discussed Lastly, some 3-D examples for aerodynamic shape optimisation works based on the proposed design methodology are presented
ISSN
0011-748X
URI
https://hdl.handle.net/10371/190204
DOI
https://doi.org/10.14429/dsj.60.581
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