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Published in 2018 at "CEAS Aeronautical Journal"
DOI: 10.1007/s13272-018-0342-z
Abstract: Based on a quasi-steady mission in a vertical plane, this paper presents an analytical derivation to compute the fuel consumption sensitivity. Within the mission analysis simplifications required by this method, a wing aerostructural design problem…
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Keywords:
consumption sensitivity;
fuel consumption;
wing aerostructural;
optimization ... See more keywords
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Published in 2017 at "Journal of Aircraft"
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,…
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Keywords:
aircraft;
aerostructural optimization;
range;
wing aerostructural ... See more keywords