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Old 6th Apr 2011, 21:13
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Jane-DoH
 
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M2Dude

3) A third isentropic fan shock is generated from the progressively
curved section of the fwd ramp
What's an isentropic fan-shock?

5) A terminal shock system is generated by the coalescence of
still supersonic and now subsonic air at the upper section of the ramp
area.
So the lower lip forms a normal shock and the airflow goes subsonic immediately behind it, the supersonic flow above somehow collide and form a shock between the ramps? I understand how the subsonic and supersonic flow coming together would reduce the average velocity -- I'm still surprised the gap between the forward and rear ramps wouldn't act like a divergent surface and cause the supersonic flow to accelerate rather than come down to subsonic speed.
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