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|Title:||Design of wing-body configurations to delay the onset of vortex asymmetry||Authors:||Cai, J.
|Issue Date:||2006||Citation:||Cai, J.,Tsai, H.-M.,Luo, S.,Liu, F. (2006). Design of wing-body configurations to delay the onset of vortex asymmetry. Collection of Technical Papers - AIAA Applied Aerodynamics Conference 2 : 1187-1208. ScholarBank@NUS Repository.||Abstract:||The stability analysis developed by Cai, Liu, and Luo (J. of Fluid Mech., vol. 480, 2003, pp.65-94) is augmented by a numerical conformal mapping technique in order to extend its applicability to problems with complex geometry. The extended method is applied to investigate the stability of symmetric vortices over wing-body combinations with various designs of the cross-sectional geometry through morphing a basic profile formed by a flat-plate wing and a circular-cone center-body. The effect of the thickness of the wing and the body, bending the wing tips, and contouring the cross-sectional proflies of the wing and the body are studied systematically. Through this process, it is discovered that a cross-sectional profile like that of a disturbed cobra has the largest stability range up to very high angles of attack for the symmetric vortices over a slender conical forebody.||Source Title:||Collection of Technical Papers - AIAA Applied Aerodynamics Conference||URI:||http://scholarbank.nus.edu.sg/handle/10635/116061||ISBN:||1563478129||ISSN:||10485953|
|Appears in Collections:||Staff Publications|
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