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![]() Stefan wrote: Of course the effects of the P-factor can be overcome by appropriate design. The most simple solution would be the possibility to trim all three axis. Yaw damping does wonders in the Pilatus. Of course your typical GA aircraft doesn't have 1200hp - and doesn't cost $3.5M. On the more expensive level (much more expensive, I would guess), you can overcome the P-factor effects by using two contra-rotating coaxial propellors. This would not only overcome the effects of the P-factor, but also those caused by torque. Kamov helicopters are an example of such a design. Effective, yes, but very complex, heavy and expensive. I recall seeing an ad for Breitling watches that had a P-51 with contra-rotating props. I think it was a one-off aircraft with a RR Griffon engine? Contra-rotating coaxial propellors not only solve the P-factor and torque, but they make the propellor more efficient, too. Probably too little effect compared to the additional cost and complexity, so it has been realized only rarely. Tupolev 114 is an example. IIRC Tu-95/114 was the fastest prop aircraft of its category. I think the cruise speed was near 500mph? I think that was a combination of high-shp Kuznetsov turboshafts and the efficiency of the contra props. Pretty amazing aircraft IMO. |
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"Kingfish" wrote in message
Effective, yes, but very complex, heavy and expensive. I recall seeing an ad for Breitling watches that had a P-51 with contra-rotating props. I think it was a one-off aircraft with a RR Griffon engine? That aircraft was modified for Unlimited racing at Reno. It also had the bobbed canopy and clipped wings. D. |
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