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