For my university project I am calculating the performance of a UAV however I am struggling to calculate the dynamic and static thrust produced by a prop. Which leads me to a couple of questions...
1) When calculating the thrust of a motor with a prop, how do I determine the RPM of the motor with a prop (adding load to a prop)?
2) Are there any calculations I can do to determine the ideal prop size without having to do any physical tests?
3) What is the most accurate dynamic thrust and static thrust equation I can use to calculate the thrust of my motor with a prop?
Motor specs:
kV = 1070; V = 11.1; unloaded RPM; 11877
Battery Specs:
3 Cell LiPo battery of 2200mAh of capacity.
If someone could help me out that would be awesome!
1) When calculating the thrust of a motor with a prop, how do I determine the RPM of the motor with a prop (adding load to a prop)?
2) Are there any calculations I can do to determine the ideal prop size without having to do any physical tests?
3) What is the most accurate dynamic thrust and static thrust equation I can use to calculate the thrust of my motor with a prop?
Motor specs:
kV = 1070; V = 11.1; unloaded RPM; 11877
Battery Specs:
3 Cell LiPo battery of 2200mAh of capacity.
If someone could help me out that would be awesome!