
Originally Posted by
skrap1r0n
On a similar vein, I have often wondered why there was a fear of the sound barrier when simple observation would reveal that the tips of propeller blades regularly exceeded the speed of sound.
Is this true??? I was under the impression that the forward speed of helicopters was limited to speed of sound minus the rotational speed of the blade tips. This, so that on their forward trip in the rotation, the blade tips would not break the sound barrier and create shock waves.
If this is in fact true, I would think the much shorter blades of a plane prop would also need to remain below the barrier for the same reason. Or, is it because they're so much shorter that their able to withstand the shockwave(s) created?