Terry
Newbie
Continuing
Continuing
Are you suggesting perhaps the MT03 tail should be larger for this reason, or would this have happened anyway?
Counter-rotating propellers would be novel, and perhaps not much more expensive than current single propeller gear boxes and blades, and with more thrust. Perhaps, instead of gearing down, use two smaller propellers at full RPM, but counter rotating. Less expensive propellers and no more expense for the gearbox.
What about thinking of ways to build in greater resistance to operator induced rotor unloading in the first place? Horizontal stabilizers help protect against instability, but is there a design criteria which can make it near impossible to induce rotor unloading without compromising performance? Why was this pilot able to take his MT03 into this condition?
Continuing
A single full span vertical or horizontal tail does a fair job of removing the swirl from the propeller slipstream and balancing torque without differential incidence. In doing so, it also recovers some of the power wasted in rotating the slipstream; the sailboat effect.
If there is no swirl of the slipstream, there is no torque reaction; counter rotating props or aerodynamic vanes to remove the swirl, for instance.
Are you suggesting perhaps the MT03 tail should be larger for this reason, or would this have happened anyway?
Counter-rotating propellers would be novel, and perhaps not much more expensive than current single propeller gear boxes and blades, and with more thrust. Perhaps, instead of gearing down, use two smaller propellers at full RPM, but counter rotating. Less expensive propellers and no more expense for the gearbox.
What about thinking of ways to build in greater resistance to operator induced rotor unloading in the first place? Horizontal stabilizers help protect against instability, but is there a design criteria which can make it near impossible to induce rotor unloading without compromising performance? Why was this pilot able to take his MT03 into this condition?