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 |
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Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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