Flow Studies on a Hydrogen-Fueled Cavity Flame-Holder Scramjet
This work extends an investigation into the use of a cavity flameholder to aid scramjet combustion at high flight Mach number. A parallel scramjet duct incorporating a cavity flame holder in the floor with an inclined rear face and an aspect ratio of 4.8
|Collections||ANU Research Publications|
|Source:||OH PLIF Imaging of Supersonic Combustion Using Cavity Injection|
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