Add general profile based elements for Z, I, T, Omega stringers

[GoogleCodeExporter]

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]

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]

add documentation picture from Felix

Original comment by daniel.b...@googlemail.com on 30 Oct 2012 at 2:16

[GoogleCodeExporter]

Issue 221 has been merged into this issue.

Original comment by daniel.b...@googlemail.com on 30 Oct 2012 at 2:34

[GoogleCodeExporter]

Included information in the documentation

Original comment by daniel.b...@googlemail.com on 30 Oct 2012 at 2:34

• Changed state: Done