"Simon Brooke" <[email hidden]> wrote in message
news:[email hidden]...
Quoted message said:in message <[email hidden]>, LSMike
(') said:"Simon Brooke" <[email hidden]> wrote in message
news:[email hidden]...
Quoted message said:in message <[email hidden]>,
Quoted message said:Helicopters can fly at at most not quite half the speed of sound for
exactly this reason.
Not quite, I think the record is some 400km/hour (that's gone up since
I
last read). I thought the main limiting factor was the reducing lift
from the retreating blades.
The speed of sound is 1,237Km/h.
Depends on the conditions, surely?
Quoted message said:The limiting factor is putting the tips
of your rotor blades through mach 1, because the stresses involved
would break them.
I rather think it's much more complex than this. I'm sure it's possible to
make rotor blades that can go faster than the speed of sound since under
certain conditions the tips of some aircraft propellers will go supersonic.
IANAE but I seem to remember that there are all kinds of aerodynamic
disadvantages to having part of a wing (i.e. rotor blade) super sonic and
part not.
Quoted message said:You do need to adjust the pitch of the retreating
blades, because going relatively slower they need to have courser
pitch.
IIRC here is the problem. Low blade airspeed and coarse pitch on the
retreating blade = stall over some of the inner (and thus slower moving)
part of the blade. The faster you go the further out the stalled section
moves. Hence I still believe this is the limiting factor.
Quoted message said:But if the advancing blades could exceed the speed of sound
without difficulty, then there would be no problem in spinning the
rotor so the advancing blades were running at (say) mach 5, the craft
was doing mach 3, and the retreating blades would still be doing mach 1
relative to the air. The reason you can't do this is as I stated.
--
[email hidden] (Simon Brooke) http://www.jasmine.org.uk/~simon/
Wannabe a Web designer?
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