Occurs in xPath:
/cpacs/vehicles/aircraft/model/wings/wing/componentsegments/componentsegment/str
ucture/ribsdefinitions/ribsdefinition
/cpacs/vehicles/aircraft/model/wings/wing/componentsegments/componentsegment/str
ucture/spars and /cpacs/vehicles/structuralelements/
Problem/Question:
Ribs and Spars 2
Comments:
Is it an idea to let the user choose between predefined rib and spar
definitions (e.g. the way the spar definition is at the moment having 1/2 webs,
an upperCap, lowerCap and rotation) and a self-designed rib or spar definition
using a structural profile defined within profiles/structuralProfiles and
linking this via UID's in the structure definition of the wing (within
componentSegments)? For the latter option, the arbitrary cross-sections can be
designed in a 0-1 square box and it has to incorporate the possibility to state
if a dimension has to be explicitly assigned a value (e.g. x-dimension = width)
or if a dimension has a 'filling' option (e.g. the y-dimension having a
'filled' option means the cross-section is filled from lowerSkin to upperSkin).
Reply:
wontFix, as it is to general
daniel.boehnke@dlr.de
Original issue reported on code.google.com by daniel.b...@googlemail.com on 25 Jan 2012 at 10:57
Original issue reported on code.google.com by
daniel.b...@googlemail.com
on 25 Jan 2012 at 10:57