Rotor Speed
#1
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Senior Member
Has anyone ever checked the rotor speed of their machine? I just got back from the field made two nice flights on my Kellet The AK-2 There was a helicopter pilot there and he had a optical tach and he used it to check my in flight rotor speed This is a rotor with 36 inch Aerobalsa blades that I cut down to 2 1/2 inches wide I cut the undercamber off of the 2 3/4 inch blades Well on a slow pass the blades were turning 670 RPM on a high speed pass 820 RPM I would be interested to know if anyone has any comparable numbers There was a wind around 12 mph and passes were into the wind
#2
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From: Le Havre, FRANCE, METROPOLITAN
900 rpm on the sparky (650g, SG6062, 1deg incidence), pretty stable. approx 600-700 rpm on the Pitcairn PA22 from A Co Az (1750g, clark Y, 1.5 deg incidence). And around 500 RPM on the Kirara (1850g, airfoil ?), which is too slow except if you increase tip weight.
For comparaison, a full size Magni M16 fully loaded has its rotor turning at approx 380 rpm (420 kg).
The rotor of the 1/10e C30 runs at 600 rpm (Weight 550g) with scaled blades (Rotor diameter 113 cm, clark Y, 1.5 deg incidence).
I recorded my BEGI between 1000 to 1100 rpm (Aerobalsa blades).
The problem is that rotor speed is highly dependent on airfoil, blade incidence, giro weight and blade shape. 1 degree less in incidence can cause the speed up by 100 to 200 rpm. Same if airborn weight increase or lift coefficient of airfoil is lower.
For comparaison, a full size Magni M16 fully loaded has its rotor turning at approx 380 rpm (420 kg).
The rotor of the 1/10e C30 runs at 600 rpm (Weight 550g) with scaled blades (Rotor diameter 113 cm, clark Y, 1.5 deg incidence).
I recorded my BEGI between 1000 to 1100 rpm (Aerobalsa blades).
The problem is that rotor speed is highly dependent on airfoil, blade incidence, giro weight and blade shape. 1 degree less in incidence can cause the speed up by 100 to 200 rpm. Same if airborn weight increase or lift coefficient of airfoil is lower.
#4
Hi Al...
The article that Les Garber and I published in RC Modeller, August 2001 has some data we recorded in our wind tunnel tests at the U of Minnesota tunnel. If you don't have a copy, I can send you one. (let me have your surface mail address.)
Bill
The article that Les Garber and I published in RC Modeller, August 2001 has some data we recorded in our wind tunnel tests at the U of Minnesota tunnel. If you don't have a copy, I can send you one. (let me have your surface mail address.)
Bill



