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17: Folder Total-Polars Computation

In the folder 'Design Computation' one can compute single flight conditions and look at the results, eventually collect an record them. Quite inconvenient, if one has to compute a series of flap deflections. Better leave this to the computer. In the following is described, how this stupid work can be automatised.
Therefore are two major functions available in the folder 'Total-Polars Computation'.
1) Flap Computations:
In this subfolder one can make pre-settings for the flap groups and the range of flap deflection angels, for which the computations are to be performed.
2) Computation of AoI-difference:
This function is intended for multi-fixed-wing aircrafts. In this subfolder wings and a range for angles of incidence can be defined for the computations.




17.1: Flap Computations
17.2: Angle of Incidence Computation
17.3: Viewing Polars as Table or Graphic

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