New Methodology for Robust-Optimal Design with Acceptable Risks: An Application to Blended/Wing/Body Aircraft

In this paper, a new design methodology guaranteeing optimal performance and constraint satisfaction with acceptable risks is presented. This methodology is particularly tailored to conceptual design, wherein variability stemming from modifications that will inevitably occur in downstream design pha...

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Veröffentlicht in:	AIAA journal 2022-05, Vol.60 (5), p.3048-3059
Hauptverfasser:	Aubeelack, Hema, Segonds, Stéphane, Bes, Christian, Druot, Thierry, Bérard, Adrien, Duffau, Marylène, Gallant, Guillaume
Format:	Artikel
Sprache:	eng
Schlagworte:	Blended-Wing-Body aircraft Constraints Design modifications Design optimization Drag Optimization Parameters Pitching moments Planforms Quadratic programming Risk levels Robustness (mathematics) Wing span
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