Originally posted by krumly
Bottom line, it's about apparent wind at the kite. Basic equations that applies to lift on a wing or thrust from a propeller (same thing, different
orientation):
Force = Air Density/2 x Area x Velocity ^2 x Lift Coefficient
Power = Air Density/2 x Area x Velocity ^3 x Lift Coefficient
Projected area affects linearly. Double area and you double lift force or pull/tension on lines.
Lift Coefficient is dependent on airfoil section, aspect ratio of wing, and angle of attack. Has a linear affect on force and power.
Apparent wind speed affects force as square of wind speed; power as cube of wind speed.
Tell me which factor matters most if you have a need for speed...
krumly |