Review of cavity ignition in supersonic flows

The cavity-based flameholder is a promising device in supersonic combustion issues in a scramjet engine and it also provides a favorable ignition environment inside the cavity owing to low speed recirculation flows and relatively high static temperature. The cavity ignition process as the beginning...

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Veröffentlicht in:	Acta astronautica 2019-12, Vol.165, p.268-286
Hauptverfasser:	Cai, Zun, Wang, Taiyu, Sun, Mingbo
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft safety Cavity flow Cavity fueling Cavity geometry Current ignition techniques Flow field Igniter setup Ignition Low speed Reacting flow Supersonic aircraft Supersonic combustion Supersonic combustion ramjet engines Supersonic flow
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