Abstract
The procedure for wing aerodynamic design based on the algorithm of simultaneous multiregime optimization of cruise and low-speed performance is considered. The method is based on the combination of fast direct methods for subsonic and transonic wing analysis, geometry variation module and the optimization procedure. The description of all the components and examples of practical application of the developed technique for design of the conventional medium-haul airplane wing and the ‘Flying Wing’ configuration are presented.
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Schedule a callMore From: ARCHIVE: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 1989-1996 (vols 203-210)
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