On morphing wing for roll augmentation via material fitness using surrogate modelling

摘要: This research is concerned with the design and analysis of a multi-camber morphing wing that meets prescribed aerodynamic configurations according to intent. A global optimisation paradigm used towards interlinks enhancement via material fitness efficient structural shape optimisation. heuristic approach proposed in this work combines both airfoil wing-morphing derivations. Based on non-linear solutions, flexible airfoils allow multiple changes through an array cambers, so flow improvements can be achieved. The argument then extended control three-dimensional wings remit enhance roll control. employs hierarchical strategy interleaving model parametrisation into analysis; and, conjunction approximation technique, augmentation investigated whilst total drag minimised.