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Aerodynamic forces cause vibrations at the tip of a blade where the effects of transonic speeds cause buffeting and vibration.
It is primarily intended to benefit aircraft that operate in the transonic speed range.
This isn't to make the aerodynamics of a trans-sonic aircraft sound simple - a lot more is going on with the airflow - but I hope it's enough to answer your question.
You don't want an arm sticking out when you go from transonic to supersonic.
When a bullet in free flight is in transonic velocity range both above and below the speed of sound, it's subject to forces detrimental to accuracy.
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