@CWilkinson :
Ramjet means subsonic then supersonic flow acceleration, hence a convergent-divergent section.
Aft of the turbojet, there is only an expension nozzle available (at leat, that I can see). We can then confirm that their burner(s) are wrapped around the turbojet engine
But today, they are probably something else than a canular design. Look at the ramjet ignition. It looks like it doesn't mind much to have a sudden start, with a rapidly accelerating flow field at a fairly low Mach number (they are not inside a Supersonic wind tunnel - the exhaust is also very Yellow bright (while the turbojet's exhaust flame was lean blue like hell)).
The flame is also separated, meaning that the combustion is dissimilar from left and right and not sourced from an axial ignition.
The universal flame coloring suggests a flaming process that is constant, instantaneous, volume restrained and... Well, let's have them come forward when they are ready.
Ramjet means subsonic then supersonic flow acceleration, hence a convergent-divergent section.
Aft of the turbojet, there is only an expension nozzle available (at leat, that I can see). We can then confirm that their burner(s) are wrapped around the turbojet engine
But today, they are probably something else than a canular design. Look at the ramjet ignition. It looks like it doesn't mind much to have a sudden start, with a rapidly accelerating flow field at a fairly low Mach number (they are not inside a Supersonic wind tunnel - the exhaust is also very Yellow bright (while the turbojet's exhaust flame was lean blue like hell)).
The flame is also separated, meaning that the combustion is dissimilar from left and right and not sourced from an axial ignition.
The universal flame coloring suggests a flaming process that is constant, instantaneous, volume restrained and... Well, let's have them come forward when they are ready.
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