...David Manuel Judt; Craig Lawson Purpose – The purpose of this paper is to present a new computational framework to address future preliminary design needs for aircraft subsystems. The ability to investigate multiple candidate technologies forming subsystem architectures is enabled...

... be the only ones considered for the aerodynamic behavior. Optimization High‐lift Evolutionary algorithm RANS CFD Aircraft Industrial design The Design, Simulation and Flight Reynolds Number Testing for Advanced High‐Lift Solutions (DeSIReH) project is funded by the European Commission...

.... The purpose of this paper is to show that the Class‐Shape‐Refinement‐Transformation method in combination with an Euler/adjoint solver provides an efficient and intuitive way of optimizing aircraft shapes. Design/methodology/approach The Class‐Shape‐Transformation method was used to parameterize...

...M. Vázquez; A. Dervieux; B. Koobus Purpose To propose an integrated algorithm for aerodynamic shape optimization of aircraft wings under the effect of aeroelastic deformations at supersonic regime. Design/methodology/approach A methodology is proposed in which a high‐fidelity aeroelastic...

...) consists of (a) a set of sensors, (b) a control unit; and (c) a set of actuators. Each ANCS is application specific, i.e. it is designed for a specific case (i.e. for the same type of car, or the same type of aircraft). During the development of an ANCS for an application, all the three basic...