PPRuNe Forums - View Single Post - MR/TR compared with Coaxial Aircraft Design
Old 15th November 2006 | 18:15
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Dave_Jackson
 
Joined: Apr 2003
Posts: 1,635
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From: Vancouver, BC, Canada
Question

?
Nick sez;
TR's "lose" about 3% of the power that the helo has.
CRAN sezed;
Representatives of the Kamov company have been present at the last two big UK Helicopter technical get-togethers and on both occassions have claimed that the co-axial rotor configuration, when properly designed is in fact more efficient than a single main rotor and tail rotor configuration. To the tune of about 15%!
Western spin versus Eastern spin?

More spin.
Dave
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