Reference Library
Technical deep dives
Paul Martin on props, motors, etc.
tbd
tbd
Batteries
TBD: https://www.facebook.com/photo/?fbid=4847037825319536&set=g.668143127181552
Motors
Stator laminations: Without super thin stator lams, efficiency suffers at high RPMs. Since thin stator lams are expensive, cheap motors (e.g. Freerchobby) use 0.35mm lams. Eddy losses in the iron stator core induced by the magnetic field switching as the rotor magnets fly past are proportional to the square of the lamination thickness x the square of the rpm. This explains why motors with thick stator lams generate excessive heat without going any faster. One notable exception is the inexpensive Turnigy Rotomax 150 which uses 0.2mm lams.
Props
Paul Martin’s documentation
4th root equation
Dr. Raynor’s equation
eCalcs
Calculators
Motor
Static thrust and horsepower
Formulas
Kv(v) = RPM
max kw - (.30) = max continuous power
Motor efficiency: Used power - heat. Heat is P=i squared * amps (resistance squared times amps)
Propeller
Prop pitch recommendation (for cruise?) based on RPM, airspeed, and prop length. You can also view the tables
Mejzlik calculators for disk loading, dynamic thrust, static thrust
Aviation
Entire power train
Metals
Flying strategies
Best climb angle and speed