Am I correct in my assumption that when sensors are applied a vacuum is formed & remains so until a crack occurs in flight while under stress which may close when the aircraft is no longer under stress & the sensor will provide that information when testing occurs.
If that is the case SMN would have a great advantage over any other system that would rely on a crack being present during testing.
At one point in time, I think it was mentioned that sensor information may be able to be transferred directly to the cockpit during flight rather than waiting for testing on the ground. I think that technology would be brilliant but could be many years down the track.
Am I correct in my assumption that when sensors are applied a...
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