Hello guys . He is playing with you and you are falling for it .
He is side tracking you .
We are talking about can blackbird can go faster than tail wind .
He has mentioned SO Far :: Inductors . because they store energy
.Yes, Not that energy that blows a ship across the water.
Turbine on a car . Yes .. Wind turbine blade for a small blade is about 25 mtr dia .. does the blade stand still & the car rotate?
Now push bikes .
This is even Funnier than
Monty Python's Flying Circus Now he has realized that he has
ed up . And drawing you All into his warped web of confusion .
And Now for something completely Different .. Reality
key parameters in propeller design, the main ones being the power to drive the propeller,
and the thrust that the propeller delivers.
• The angle between blade chord and propeller plane is the geometric pitch (blade angle β
• )
• Angle of attack of the blade element α=β−Φ
• The effective pitch angle is Φ=arctan(V/ω∗r)
. This is often given relative to rotational speed n = rounds per second of the propeller, and the propeller diameter R:
Φ=arctanVn⋅D∗1π⋅r/R
The advance ratio J of the propeller is
J=Vn⋅D
Induced velocity should be constant over the blade, implying that β
decreases linearly with increasing r: the propeller blade twist. Because the twist changes linearly, one point on the blade can be taken as the representative blade β
, and this is usually taken at either 70% or 75% of the radial distance.
It can be shown that for a given blade geometry, the power and thrust coefficients CP
and CT of the propeller are determined only by J and β0.75. If tip speed is below speed of sound and the blades are not stalled, Mach and Reynolds number effects are negligible.
CP=Pρ⋅n3⋅D5
CT=Tρ⋅n2⋅D4
now look up CP
as function of J in for instance NACA reports from the NACA
Regarding the profiles: propeller design is pretty specialist but old fashioned NACA profiles are still being used in helicopter blades for both main rotor and tail rotor. (Example) For a symmetrical profile NACA 0012 would be a representative choice, again available from the NASA .
A reference book on this is Theory Of Wing Sections by Abbott & Von Doenhoff.
Sorry if I am a bit rusty the last design stuff was over 45 years ago .