Numerical Algorithm for Wing-Structure Design

TL;DR: In this article, a numerical method for minimising induced drag with structural constraints is presented that uses approximations that apply to unswept planar wings with arbitrary planforms and weight distributions.

TL;DR: In this paper, a transonic supercritical wing design is developed with aerodynamic characteristics that are well behaved and of high performance for configurations with and without the nacelle/pylon group.

TL;DR: In this paper, a multi-point high-fidelity aerostructural optimization of a long-range wide-body transonic transport aircraft configuration is presented, where the coupled adjoint sensitivity method is used to efficiently compute gradients, enabling the use of gradient-based optimization with respect to hundreds of aerodynamic shape and structural sizing variables.

TL;DR: In this paper, an integrated aerostructural method for the design of aerospace vehicles is presented, where both aerodynamic and structural structures are represented using high-fidelity models such as the Euler equations for the aerodynamics and a detailed finite element model for the primary structure.

TL;DR: In this article, an introduction to hydrodynamics is given, which is designed to give those who have not yet been actively concerned with this science such a grasp of the theoretical underlying principles that they can follow the subsequent developments.