"Tom probably did pick up 20 mph. I would not know. However i do know this, Mike, the original poster will not have the same Horsepower that Tom does while he races at Reno, He will have about 200 HP. If you have more HP than 2 blades can handle, go to 3, or 4 or whatever, just like the WWII fighters did. But if you have 200 HP then 2 blades will do it. If all it took were more blades to go faster, then i would put about 200 of them on my plane and really go!"
steve ciha
Steve, you're missing my point. Properly-designed multi-blade props have no more loss than does a two-blade prop. By taking advantage of the greater amount of air being pumped at an even smaller diameter, a multi-blade prop can be even slightly more efficient than a two blade, and will give more static thrust and better climb. Certainly, higher HP engines require more and fatter blades to keep diameter/rpm in a reasonable range. But the three and four blade props on Tom's IO-360 plane were less than 60" in diameter! Jim Smith's 150HP RV-6 with its three-blade "bow tie" prop goes 192 mph TAS at 7000' dalt at 2740 rpm. My Lancair has only a 125 HP O-235, yet it's takeoff and climb with my three-blade is better than a two-blade, yet I get 214 mph TAS at 1000' dalt and 200 mph TAS at 10,000 dalt. I'm just trying to show that a multi-blade prop that doesn't have as good a cruise speed as a two-blade is because it has a poor blade design, not because it has more blades! It has been very difficult for me to get across that these popularly-held notions of prop diameter, number of blades, and blade thickness have often been in opposition to the truth! Long-held, incorrect popular notions die hard! Another of these is that the curved-divergent submerged duct, the "NACA duct", is the best in every application! I designed some much smaller inlets to replace NACA ducts on some Reno racers that gave much more air for intercoolers and cabin ventilation.