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14.10: Computed Values

After a successful vortex computation there are not only the design input fields filled with values, but a lot more data is made available by the program. Click the button 'Computed Values' to open a new window.



In this window you will find the results of the vortex computation in a general survey. In the following, the 'Computed values' are explained in details. Depending on the number of wings two ore more folders are shown. The first folder holds the data for the entire airplane.



To the right the folders for the individual wings follow, in each case with number and designation of wing. In the folders of the wings you will also find local coefficients for the panel stripes along the span of wing. The marked line indicates the panel stripe on which the marking bar in 2D-graphic is located.
Minimize the window 'Computed vales' a bit, and shift it to a position on screen, that you can see the 2D-graphic window. Press the left mouse button and move the mouse cursor over the 2D-graphic window. The line marker in the window 'Computed vales' follows these movements. Thus you can examine all local values of the selected panel strip.




Click the button 'Save As...' to store the computed data in a text file.

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