Multidisciplinary Analysis of CROR Propulsion Systems: DLR Activities in the JTI SFWA Project

Abstract

In the frame of the EU 7th Framework Joint Technology Initiative Smart Fixed Wing Aircraft project, the DLR Institute of Aerodynamics and Flow Technology (DLR-AS) is participating as an associated partner in the Airbus-led studies of the Contra-Rotating Open Rotor as possible powerplant for future transport aircraft. Due to significant technical challenges in terms of noise emissions, installation effects and certification that still need to be addressed for this novel propulsion system, the numerical activities require the use of sophisticated multidisciplinary analysis tools and approaches covering aerodynamics, aeroacoustics and aeroelastics. In this paper an overview of the DLR-AS work in the project is given, which covers the numerical assessment of a novel noise reduction technology, the investigations of the impact of blade deformation on aerodynamic performance and noise emissions as well as some in-depth studies on isolated and installed pusher-configuration CROR engines and the validation of these simulations using experimental test data that is being generated in Airbus-led low- and high-speed wind tunnel tests.