Details of the Cyclon .40 PR Pylon Racing Engine |
Performance Data |
Propeller | Dia | Thrust Coeff. | Power Coeff. | RPM | Density | Power | Thrust |
---|---|---|---|---|---|---|---|
D [m] |
Ct 0 [-] |
Cp 0 [-] |
n [1/min] |
r [kg/m³] |
P 0 [W] |
T 0 [N] |
|
R1 Rüdiger Keck | 0.185 | 0.1249 | 0.0697 | 25050 | 1.195 | 1295 | 30.1 |
0.185 | 0.1249 | 0.0697 | 25600 | 1.205 | 1394 | 31.8 | |
0.185 | 0.1249 | 0.0697 | 26000 | 1.208 | 1464 | 32.8 | |
F1 Olivier Allais | 0.182 | 0.1298 | 0.0899 | 17000 | 1.205 | 492 | 13.8 |
F1 (Nelson engine) | 0.182 | 0.1298 | 0.0899 | 25900 | 1.208 | 1744 | 32.1 |
S1 Sasha Smoletsev | 0.178 | 0.1353 | 0.0946 | 25200 | 1.208 | 1512 | 28.9 |
A1 Ranjit Phelan | 0.187 | 0.1249 | 0.0923 | 24000 | 1.208 | 1610 | 29.2 |
V1 Verano Copy | 0.188 | 0.0999 | 0.0820 | 26000 | 1.205 | 1887 | 28.2 |
0.188 | 0.0999 | 0.0820 | 25600 | 1.208 | 1806 | 27.4 | |
0.188 | 0.0999 | 0.0820 | 25800 | 1.208 | 1849 | 27.9 | |
0.188 | 0.0999 | 0.0820 | 25890 | 1.195 | 1848 | 27.8 | |
0.188 | 0.0999 | 0.0820 | 26000 | 1.208 | 1892 | 28.3 | |
Remarks: - The trailing "0" means "static condition" i.e. v = 0. - The engine was running on 80/20 FAI fuel during all my tests. - Weather conditions were close to standard conditions, corrections were below measurement accuracy. - the propeller coefficients were determined by wind tunnel tests. |
My test results and another performance curve, taken from a
japanese web site (forgot to bookmark that page, though).
The test data matches the performance curve found on the japanese web page quite well. The data was taken using propellers, which were calibrated in a wind tunnel. It is possible, that the calibration data of the R1 prop are a bit on the low side concerning power input, due to Reynolds number differences.
Some Technical Data |
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|
Mounting Dimensions |
Dimensions of a plate to mount the Cyclon 40 on my test bench.
Photo Gallery (click on the photos to enlarge) |
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Last modification of this page: 21.05.18
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