Wing Aerostructural Optimization Under Uncertain Aircraft Range and Payload Weight
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DOI: 10.2514/1.c034050
Abstract: An uncertainty-based approach is undertaken to deal with multipoint wing aerostructural optimization. The flight points are determined by the quadruple set of parameters: Mach number, cruise altitude, carried payload, and flight range. From this set,… read more here.
Keywords: aircraft; aerostructural optimization; range; wing aerostructural ... See more keywords