TY - GEN
T1 - Integrated multidisciplinary aircraft design process supported by a decentral MDO framework
AU - Daoud, Fernass
AU - Deinert, Sebastian
AU - Maierl, Reinhold
AU - Petersson, Ögmundur
N1 - Publisher Copyright:
© 2015 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2015
Y1 - 2015
N2 - Since aircraft design is inherently multidisciplinary, the exploitation of the interaction of the design-driving disciplines and physical phenomena opens the door for new design spaces and consequently new high-performing solutions. However, the key driver is to make these potentials accessible in the conceptual design of the aircraft, where the main aircraft configuration decisions are taken. In response to these challenges Airbus Defence and Space is developing an integrated air vehicle design process based on multidisciplinary and decentral IT framework enabling, on the one hand, shifting the focus in conceptual design from using statistics, especially if no statistics are available for an unconventional design, towards simulation assisted conceptual design on the basis of automatically generated numerical analysis models, and on the other hand, a seamless fidelity level of applied methods, tools and numerical simulation models between the concept design phase and subsequent design phases (preliminary, detailed, etc.).
AB - Since aircraft design is inherently multidisciplinary, the exploitation of the interaction of the design-driving disciplines and physical phenomena opens the door for new design spaces and consequently new high-performing solutions. However, the key driver is to make these potentials accessible in the conceptual design of the aircraft, where the main aircraft configuration decisions are taken. In response to these challenges Airbus Defence and Space is developing an integrated air vehicle design process based on multidisciplinary and decentral IT framework enabling, on the one hand, shifting the focus in conceptual design from using statistics, especially if no statistics are available for an unconventional design, towards simulation assisted conceptual design on the basis of automatically generated numerical analysis models, and on the other hand, a seamless fidelity level of applied methods, tools and numerical simulation models between the concept design phase and subsequent design phases (preliminary, detailed, etc.).
UR - http://www.scopus.com/inward/record.url?scp=85088356354&partnerID=8YFLogxK
U2 - 10.2514/6.2015-3090
DO - 10.2514/6.2015-3090
M3 - Conference contribution
AN - SCOPUS:85088356354
SN - 9781624103681
T3 - 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
BT - 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015
Y2 - 22 June 2015 through 26 June 2015
ER -