Appendix
Calibrate Thrust Tc = 0.411*(T-T0) Calibrated Thrust(g) = 0.411 * (Thrust
scale reading(g)-Thrust scale reading at
0% power(g))
Power Input Pin = V*I*(P%/100) Power Input(w) = Voltage(v)*current(A)
*(Arduino Power Setting/100)
Power Available Pout = Tc*v Power Available(w) = calibrated
thrust(N)* wind tunnel velocity(m/s)
Propulsion Efficiency nsys = Pout/pin *100% propulsion Efficiency(%) = power output
(w)/power input(w) *100%
Propeller Advance J = v/(RPM/60)*D Propeller Advance(J) = velocity(m/s) /
((Propeller RPM /60)*Propeller diameter(m))
1 Mark = 0.4875 inches
Code
motorSpeed(4,25); //constant speed for all at 25%
goFor(2); //hold for 2 sec
motorSpeed(4,20); //constant speed for all at 20%
goToAbsolutePosition(332.3); //go 332.3 marks by calculation
reverse(4); // reverse all propellers
motorSpeed(4,30); //constant speed for all at 30%
goFor(1); //hold for 1 sec
brake(4); //break all