This paper presents an extension of the Kulfan class-shape transformation method for the parameterization of aircraft component geometry. The VT-CST code represents a practical implementation of the class-shape transformation method in an object-oriented C++ code for use within a multidisciplinary design optimization framework for design studies of a tailless supersonic aircraft. Extensions to the class-shape transformation method incorporated into VT-CST include the generation of a blended wing–fuselage, cowls and inlet ramps for embedded engines, automatic handling of centerline continuity, shape normalization and scaling, fuselage area-ruling capabilities, conical cambering, airfoil shape matching, and control surfaces, among others. Examples demonstrating the utility of the method are given.
Parametric Geometry Model for Design Studies of Tailless Supersonic Aircraft
Journal of Aircraft ; 51 , 5 ; 1455-1466
2014-09-01
Conference paper , Article (Journal)
Electronic Resource
English
Parametric Geometry Model for Multidisciplinary Design Optimization of Tailless Supersonic Aircraft
British Library Conference Proceedings | 2012
|Tailless aircraft design problems
Engineering Index Backfile | 1946
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