PANUKL Help - ITLiMS

In this mode we can create fuselage geometry file for PANUKL:
Max. frame number defining fuselage geometry (frame No.0 counts in).
Number of stringers on a single frame.
Frame name syntax must be: [_.w] or [_.txt]. Where
is the number of next frame (numeration starts from frame No.0). Frame No.0 point coordinates can
be defined in .
To use [name.txt] UNIGRAPHICS files in section select NX FILES check box and specify
coordinate system for defining frame points: WCS or ABSOLUTE.
Create fuselage geometry file button.
Modification mode in FUSELAGE DATA
Fig. 74 – Modify mode in FUSELAGE program
In this mode we can modify existing fuselage geometry file. Things we can modify:
Scale fuselage. EQUAL scale FACTORS can be used in every scaling direction (X, Y, Z).
Translate fuselage. Translate to a specified X, Y, Z point location
or delta translate: DX, DY, DZ coordinate increments must be defined.
Translate fuselage only in XZ plane.
Translation type selection.
Click Modify button to accept changes and modify fuselage file.
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