Review of cavity-stabilized combustion for scramjet applications

Cavities are widely used as flameholders in supersonic combustors due to their outstanding potential to stabilize combustion without excessive total pressure loss. A review of cavity-stabilized combustion for scramjet applications is provided in this article. The topics cover the fundamental problem...

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Veröffentlicht in:	Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering Part G: Journal of Aerospace Engineering, 2014-12, Vol.228 (14), p.2718-2735
Hauptverfasser:	Wang, Zhenguo, Wang, Hongbo, Sun, Mingbo
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace engineering Combustion Correlation analysis Geometry Guidelines Holes Oscillations Pressure Propagation Scramjets Stabilization Supersonic aircraft Unsteady
Online-Zugang:	Volltext
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