Optimization of Thrust of a Generic X-51 Hypersonic Vehicle

A prune-and-search optimization algorithm was combined with a reduced-order model of the scramjet engine within a generic X-51 vehicle. The goal was to maximize the thrust in order to achieve thrust-to-drag ratios that equal or exceed 1, even for the difficult cases of flight at high altitudes and h...

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Veröffentlicht in:Journal of propulsion and power 2024-11, Vol.40 (6), p.905-915
Hauptverfasser: Choi, Yunseok, Driscoll, James F.
Format: Artikel
Sprache:eng
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