Airfoils can be described by point clouds as done in most airfoil libraries. ![]() Several approaches to parametrization of wing proles can be found in the literature. The underlying idea with this parametrization is to couple an appropriate number of parameters, balancing the need of geometric accuracy with the necessity of few airfoil parameters in order to facilitate en expedient optimisation, with the intrinsic value of having parameters that makes sense for a human such as thickness, camber and trailing edge thickness. 2013 (English) Book (Other academic) Abstract Ī fundamental part of aircraft design involves wing airfoiloptimization, establishing an outer shape of the wing which has good aerodynamic performance for the design mission, good internal volume distribution for fuel and systems and which also serves as an efficient structural member supporting the load of the weight of the aircraft.
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