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.
Multi-objective optimization procedure for the wing design at cruise and low-speed conditions
2013-02-01
12 pages
Article (Journal)
Electronic Resource
Unknown
Multi-objective optimization procedure for the wing design at cruise and low-speed conditions
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