01.1 - Aircraft Design and Integrated Systems (Theory, Methods and Tools)
A BENCHMARK FOR UNCERTAINTY QUANTIFICATION AND OPTIMIZATION UNDER UNCERTAINTY IN CONCEPTUAL AIRCRAFT DESIGN: THE F25-OUU CHALLENGE PROBLEM
B.D. Phillips¹, E. Aretskin-Hariton¹, A. DeBlois², J, Singh², M. Abu-Zurayk, German Aerospace Center (DLR), Germany; J.A. Schaefer³, S. Wakayama³; ¹NASA Glenn Research Center, United States ;²Bombardier Aviation, Canada ;³The Boeing Company, United States
This paper extends a previously published MDO benchmark problem with a comprehensive UQ and design under uncertainty formulation, providing an open, complex test case to bridge the gap between academic development and industrial adoption.
DOI: 10.71945/icas2026_0320