Sir,
I need some details of helicopters with tail rotor for my project. they are
1. is it required to maintain certain(1:6,1:3, etc)rpm ratios (main rotor rpm to tail rotor rpm) to provide effective anti-torque.
2. instead of keeping rpm ratios mentioned earlier is it enough to have sufficient thrust alone to counteract anti-torque.
3.is the thrust of tail rotor depends on these factors RPM,tail rotor blade area and shape. what are their individual contribution?
4. with minimum rpm in tail rotor is it possible to obtain high thrust for anti-torque.if so how?
5.i m designing a helicopter model with mini compression ignition engine(1.5cc) with rpm upto 16000..what is its hp and torque? to counteract main rotor torque what is the thrust required from the tail rotor(distance of tail rotor shaft to main rotor shaft is 1ft which is fixed)
i need detailed info of above question ......please reply as soon as possible
thank you in advance
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