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MJD -> RE: OS .15 CV-A question. (1/14/2010 8:20 AM)
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I partially tore down my CV15-DF or CV15-X or whatever it is - either I guess - and got a couple of measurements and pictures, so I'll put it here. I like the little plastic mount that goes into the F-86 fan shroud assembly.. it begs to be used in the front of a glass or craftily sculpted ply nose on a speed model. It could be secured easily with machine screws. Note the crank bore to carb throat ratio.. even closer than I thought. 0.245"/6.2mm crank passage, 0.235"/6.0mm carb throat, or 96%. That's about the limit.. but a 0.245" venturi may give a last few rpm, who knows. I wonder how fast this'll spin a break-in trimmed Graupner or Eliminator 6x5.5 prop.. we'll soon find out. I think they were regularly run on 30%+ nitro in the Sabres. I think I'll use something like SIG Champion 25%. BTW re the prop thing above - props use airfoils, sure, but this does not change the nature of pitch speed nor is there any weird science going on. A prop moving forward sees an AoA based on the pitch angle of the blades, the rpm and the airspeed. Wings moving forward do not produce positive lift at AoA below the zero lift angle. Similarly, aircraft in level flight do not exceed pitch speed of their own accord, because the definition of pitch speed is the speed where the relative wind approaches the prop blade airfoil at zero lift angle. Why you see examples where these quickie calculations falter is for more than one reason, IMHO: - Pitch ratings based on chord line or worse yet, the lower surface datum line like pitch gauges generally measure. These can easily be 2,3 or more degrees lower than the true aerodynamic pitch. A Clark-Y airfoil for example, flying with the chord line at zero degrees angle of attack, is actually flying at 3.52% positive AoA. A NACA 2415, like ACE wings, at 2.06 degrees positive when set up similarly. - Rounding error, i.e. is that 7" pitch prop really 6.77"? Or pure error in mfg. pitch rating. - Data error in measuring true airspeed, rpm, etc. So a "10-7" prop can mysteriously fly an airplane at 103% of pitch speed - it's just GIGO effect. IOW the calculated figure carries more significant digits than the incoming data can support. MJD
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