Numerical Simulations in Scramjet Combustion with Boundary-Layer Bleeding

Airframe-integrated scramjet engines swallow the boundary layers that develop on the forebody of space planes. The scramjet engine easily falls into engine stall (engine unstart) as a result of the boundary-layer separation resulting from combustion. In this study, to investigate the unstart charact...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of propulsion and power 2005-07, Vol.21 (4), p.642-649
Hauptverfasser: Kouchi, Toshinori, Mitani, Tohru, Masuya, Goro
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!