Abstract
Novel configuration design choices may help achieve revolutionary goals for reducing fuel burn, emission and noise, set by Flightpath 2050. One such advance configuration is a blended wing body. Due to multi-diciplinary nature of the configuration, several partners with disciplinary expertise collaborate in a Model driven ‘AGILE MDAO framework’ to design and evaluate the novel configuration. The objective of this research are: • To create and test a model based collaborative framework using AGILE Paradigm for novel configuration design & optimization, involving large multinational team. Reduce setup time for complex MDO problem. • Through Multi fidelity design space exploration, evaluate aerodynamic performance • The BWB disciplinary analysis models such as aerodynamics, propulsion, onboard systems, S&C were integrated and intermediate results are published in this report.
| Original language | English |
|---|---|
| Title of host publication | 2018 Aviation Technology, Integration, and Operations Conference |
| Publisher | American Institute of Aeronautics and Astronautics Inc. (AIAA) |
| Number of pages | 27 |
| ISBN (Electronic) | 9781624105562 |
| DOIs | |
| Publication status | Published - 2018 |
| Event | 18th AIAA Aviation Technology, Integration, and Operations Conference, 2018 - Atlanta, United States Duration: 25 Jun 2018 → 29 Jun 2018 |
Conference
| Conference | 18th AIAA Aviation Technology, Integration, and Operations Conference, 2018 |
|---|---|
| Country/Territory | United States |
| City | Atlanta |
| Period | 25/06/18 → 29/06/18 |
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