01 - Aircraft Design and Integrated Systems
STRATEGY AND IMPLEMENTATION OF A PARAMETRIC CAD MODEL FOR R2035 AIRCRAFT STRUCTURE AND EXTERNAL CONFIGURATION
Z.-J. Goraj¹, B. Goliszek¹, M. Kowalski¹, A. Seitz², F. Peter², F. Meller, Airbus Defence and Space GmbH, Germany; ¹Warsaw University of Technology, Poland ;²Bauhaus Luftfahrt e.V., Germany
CAD model for A330-300 R2035 structure and external configuration will be developed for performing a benchmarking of the optimized Propulsive Fuselage Concept design and performance. Basing on this CAD model the advanced numerical methods will be used to assess the state of strain for certification-relevant load cases according to CS-25.