I was having a discussion with a mate the other day regarding helicopter speed, or rather their top speeds. I argued that the top speed would limited by the fact the rotor blade that was moving away from the direction of travel [if the blades were rotating clockwise as viewed from above this would be the righthand side] would eventually generate negative lift as the air passing over it would be faster than it's rotaional speed. At this point I supposed the aircraft would flip over.
Later, I thought about it and reckoned you could get around the problem by having two counter-rotating blades on the same prop shaft, but then I thought this would have been tried before if it was feasable.
Anyway, my question is, if indeed this is a problem, are there any ways to overcome it.
Hope I've explained what I'm on about...
Cheers,
Shab.
Later, I thought about it and reckoned you could get around the problem by having two counter-rotating blades on the same prop shaft, but then I thought this would have been tried before if it was feasable.
Anyway, my question is, if indeed this is a problem, are there any ways to overcome it.
Hope I've explained what I'm on about...
Cheers,
Shab.
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