Does any one know accurate Lift Co-efficient of a tested and operational Rotor blade of a Helicopter?
The Lift co-efficient of a Blade depends on the
1)Forward Air speed it encounters
2)its Angle of Attack
3)The area of the Blade
4)The Weight of the Blade
I just want some accurate data of a Operational Helicopter's Blade Lift co-efficient which was recorded under the above characteristic's and environment like at what Airspeed,AOA,area of blade the CL was calculated...etc....
If anyone has,please share it with me,thank you
The Lift co-efficient of a Blade depends on the
1)Forward Air speed it encounters
2)its Angle of Attack
3)The area of the Blade
4)The Weight of the Blade
I just want some accurate data of a Operational Helicopter's Blade Lift co-efficient which was recorded under the above characteristic's and environment like at what Airspeed,AOA,area of blade the CL was calculated...etc....
If anyone has,please share it with me,thank you
