International audienceThe present paper summarizes the main results obtained from the CFD analysis of a reference boxwing configuration designed during the initial phase of the PARSIFAL project, with focus on the assessment of its aerodynamic performance in the transonic regime. For such purpose, high-fidelity RANS computations have been carried out and a detailed inspection of the different drag sources, induced, wave and viscous drag components, is presented. In addition, preliminary results from the acoustic analysis of such innovative aircraft configuration are also discussed, concerning the impact of the engine location
