The Airflow Performance manual talks about using pressure at the flow divider as a way of measuring fuel flow, which seems to me a bit simpler than the floscan 201 or redcube FT-60 turbine systems. Has anyone successfully used this pressure method? I've extracted the page below.
Thanks!
![QDd5k.jpg](/proxy.php?image=http%3A%2F%2Fi.imgur.com%2FQDd5k.jpg&hash=f7e5a1d5cdb11e4ae238e3f98aab8451)
Thanks!