
           ┃┓           ┓          ^┓
           ┃┃           ┃           ┃
           ┃┃           ┣╸dP[0]    ^┣╸1/dC_T[2]
           ┃┃           ┛ (9,235W) ^┛ (24.3)
           ┃┃           ┓          ^┓
           ┃┃           ┃           ┃
           ┃┃           ┣╸dP[1]    ^┣╸1/dC_T[2]
           ┃┃           ┛ (8,818W) ^┛
           ┃┃           ┓          ^┓
      Cost╺┫┃           ┃           ┃
 (43,582W) ┃┣╸P         ┣╸dP[2]    ^┣╸1/dC_T[2]
           ┃┃ (43,582W) ┛ (8,818W) ^┛
           ┃┃           ┓          ^┓
           ┃┃           ┃           ┃
           ┃┃           ┣╸dP[3]    ^┣╸1/dC_T[2]
           ┃┃           ┛ (8,818W) ^┛
           ┃┃           ┓          ^┓
           ┃┃           ┃           ┃
           ┃┃           ┣╸dP[4]    ^┣╸1/dC_T[2]
           ┃┛           ┛ (7,895W) ^┛



           ┃┣╸P ≥ dP[:].sum()
           ┃┛
           ┃┣╸R ≤ R_max
           ┃┛
           ┃┣╸r[4] ≤ 1
           ┃┣╸A = 3.14⋅R²
           ┃┣╸Delta_r[:].sum() ≤ 1
           ┃┣╸r[4] ≥ r[3] + 0.5⋅Delta_r[3] + 0.5⋅Delta_r[4]
           ┃┣╸V_i[0]²⋅r[0]⋅Delta_r[0]/(dC_T[0]⋅(Omega⋅R)²) = 0.25
 BEMTHover╺┫┣╸xi[0] = rho⋅A⋅(Omega⋅R)²⋅dC_T[0]
           ┃┓
           ┃┃
           ┃┃
           ┃┃
           ┃┃
           ┃┣╸[21 terms]
           ┃┃
           ┃┃
           ┃┃
           ┃┛


Optimal Cost
------------
BEMTHover.P : 4.358e+04 [W]

Solution
--------
BEMTHover
         A : 201.1     [m²]           disk area
     Omega : 16.73     [rpm]          rotor RPM
         P : 4.358e+04 [W]            total induced power
         R : 8         [m]            rotor radius
Delta_r[:] : [ 0.435     0.177     0.139     0.119     0.13     ]       non-dimensional radius step
    V_i[:] : [ 4.62      4.41      4.41      4.41      3.95     ] [m/s] induced velocity
   dC_P[:] : [ 0.0136    0.0129    0.0129    0.0129    0.0116   ]       incremental power coefficient
   dC_T[:] : [ 0.0412    0.0412    0.0412    0.0412    0.0412   ]       incremental thrust coefficient
     dP[:] : [ 9.24e+03  8.82e+03  8.82e+03  8.82e+03  7.89e+03 ] [W]   incremental power
      r[:] : [ 0.218     0.589     0.747     0.876     1        ]       non-dimensional radius
...constants
     R_max : 8         [m]     (-1)   maximum rotor radius
       rho : 1.23      [kg/m³] (-0.5) air density
    dr_min : 0.001             (~0)   minimum bin width (non-dimensional)
 Omega_max : 280       [rpm]   (~0)   maximum rotor RPM
 Omega_min : 1         [rpm]   (~0)   minimum rotor RPM
     R_min : 0.1       [m]     (~0)   minimum rotor radius
     xi[:] : [ 2e+03   2e+03   2e+03   2e+03   2e+03  ] [N]   thrust per bin (fixed)
        sens ( +0.318  +0.303  +0.303  +0.303  +0.272 )

Most Sensitive Constraints
--------------------------
BEMTHover
+1                                         : P ≥ dP[:].sum()
+1                                         : R ≤ R_max
+0.5134                                    : r[4] ≤ 1
+0.5                                       : A = 3.14⋅R²
+0.4866                                    : Delta_r[:].sum() ≤ 1
+0.4228                                    : r[4] ≥ r[3] + 0.5⋅Delta_r[3] + 0.5⋅Delta_r[4]
[ -0.318  -0.303  -0.303  -0.303  -0.272 ] : V_i[:]²⋅r[:]⋅Delta_r[:]/(dC_T[:]⋅(Omega⋅R)²) = 0.25
[ +0.318  +0.303  +0.303  +0.303  +0.272 ] : xi[:] = rho⋅A⋅(Omega⋅R)²⋅dC_T[:]
+0.2691                                    : r[3] ≥ r[2] + 0.5⋅Delta_r[2] + 0.5⋅Delta_r[3]
[ +0.212  +0.202  +0.202  +0.202  +0.181 ] : V_i[:]³⋅r[:]⋅Delta_r[:]/(dC_P[:]⋅(Omega⋅R)³) = 0.25
[ -0.212  -0.202  -0.202  -0.202  -0.181 ] : dP[:] = rho⋅A⋅(Omega⋅R)³⋅dC_P[:]
+0.1283                                    : r[2] ≥ r[1] + 0.5⋅Delta_r[1] + 0.5⋅Delta_r[2]
+0.106                                     : r[0] = Delta_r[0]/2
