05 - Propulsion
PROPULSION SYSTEM - AIRFRAME INTEGRATION AND OPTIMIZATION OF CIVIL AIRCRAFT- AGILE EU PROJECT
K.S. Anisimovš, A.A. Savelyevš, I.A. Kursakovš, A.V. Lysenkovš, A.A. Mirzoyan, CIAM, Russia; P.S. Prakasha, Institute of System Architectures in Aeronautics, DLR, Germany; šTSAGI, Russia
Civil airframe and propulsion integration is one of the complex phase of aircraft design process. Usually not considered in conceptual design process. The scope of this research is to consider the airframe propulsion matching at earlier stage of aircraft design and MDO for less fuel burn and emission, providing more knowledge and hence reducing the uncertainty for the later phases of the design.