JB77UK
3rd Oct 2011, 00:43
In airplanes LDmax (best lift to drag ratio) is the point where the wing's angle of attack is at a 'sweet spot' where it provides the most lift to drag. In an airplane that translates into the best glide speed (See FAA Airplane Flying Handbook pg3-16 for more details).
But in the helicopter, with the aerodynamic forces involved in an autorotation I'm not sure that things are the same. I have been told that LDmax for a helicopter is actually Vy speed - best rate of climb.
So I fly an R22, and I am sure most rotorheads know that helicopter, so lets take that as an example.
In the R22:
Vy (best rate of climb) is 53 KIAS
Vg (best glide in an autorotation) is 75 KIAS
So which (if any of those) is LDmax?
As a comparison, a Diamond 20 single engine airplane:
Vy 75 KIAS
Vg 73 KIAS (also identified as LDmax)
Many thanks for all contributions
But in the helicopter, with the aerodynamic forces involved in an autorotation I'm not sure that things are the same. I have been told that LDmax for a helicopter is actually Vy speed - best rate of climb.
So I fly an R22, and I am sure most rotorheads know that helicopter, so lets take that as an example.
In the R22:
Vy (best rate of climb) is 53 KIAS
Vg (best glide in an autorotation) is 75 KIAS
So which (if any of those) is LDmax?
As a comparison, a Diamond 20 single engine airplane:
Vy 75 KIAS
Vg 73 KIAS (also identified as LDmax)
Many thanks for all contributions