04 - Propulsion
INTEGRATION OF HYBRID PROPULSION SYSTEM IN A CS23 COMMUTER DESIGN
M. Stracką, T. Zillą, B. Nagelą; ąGerman Aerospace Center (DLR), Germany
Based on an existing turboprop commuter and a given propulsion system architecture, the integration of both is done. Therefore a mulitfidelity overall design synthesis is performed consisting of initialization and a higher fidelity design process. The comparison with the original aircraft performance are quantified and presented in this study.