Bug in post_stall_coefficients for numpy > 1.23

[MarcusBack]

Numpy 1.23 introduces updates to multidimensional indexing which results in error when designing propeller.

Change required on this line (remove square brackets and use numpy > operator):

SUAVE/trunk/SUAVE/Methods/Aerodynamics/AERODAS/post_stall_coefficients.py

Line 83 in f01d6a2

con3 = [alpha>=(92.0*Units.deg)]

Warning from numpy 1.22.4

 FutureWarning: Using a non-tuple sequence for multidimensional indexing is deprecated; use `arr[tuple(seq)]` instead of `arr[seq]`. In the future this will be interpreted as an array index, `arr[np.array(seq)]`, which will result either in an error or a different result.
    CL2[con3] = -0.032*(alpha[con3]/Units.deg-92.0) + RCL2*((alpha[con3]-92.*Units.deg)/(51.0*Units.deg))**N2