Reduced-Order Modeling of Two-Dimensional Supersonic Flows with Applications to Scramjet Inlets

Control-oriented models of hypersonic vehicle propulsion systems require a reduced-order model of the scramjet inlet that is accurate to within 10% but requires less than a few seconds of computational time. To achieve this goal, a reduced-order model is presented, which predicts the solution of a s...

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Veröffentlicht in:	Journal of propulsion and power 2010-05, Vol.26 (3), p.545-555
Hauptverfasser:	Dalle, Derek J, Fotia, Matt L, Driscoll, James F
Format:	Artikel
Sprache:	eng
Online-Zugang:	Volltext
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