Add general profile based elements for Z, I, T, Omega stringers
Closed this issue · 4 comments
GoogleCodeExporter commented
Xpath of the element CPACS:
"/cpacs/vehicles/aircraft/structuralElements..."
Type in CPACS:
"profileBasedStructuralElements"
What version of CPACS are you using?
"CPACS 2.0/1.6(for Fuselages)"
Please specifiy further information for your issue:
Currently, there is a profileBased definition for structuralElements. This
definition is powerful yet very general. For fast sizing processes it would be
necessary to have simple profile definitions at hand. These could be coded in
the form of typic Z, I, T and Omega stringers.
Working with engineer constants as a bypass is not meaningful as these are a
result of the sizing process.
A converter from these typic stringers to conventional profileBasedDefinitons
might be necessary.
Please provide any additional information below:
Original issue reported on code.google.com by daniel.b...@googlemail.com on 19 Apr 2012 at 8:00
GoogleCodeExporter commented
see overall Fuselage update from BK for CPACS 2.01
Original comment by daniel.b...@googlemail.com on 7 Oct 2012 at 11:44
- Added labels: milestone-CPACS2.01
- Removed labels: milestone-CPACS2.1
GoogleCodeExporter commented
add documentation picture from Felix
Original comment by daniel.b...@googlemail.com on 30 Oct 2012 at 2:16
GoogleCodeExporter commented
Issue 221 has been merged into this issue.
Original comment by daniel.b...@googlemail.com on 30 Oct 2012 at 2:34
GoogleCodeExporter commented
Included information in the documentation
Original comment by daniel.b...@googlemail.com on 30 Oct 2012 at 2:34
- Changed state: Done