Issues
- 0
Clean up Enumeration of refType
#411 opened - 0
TLAR
#410 opened - 0
Renamce forces and moments in nodalloads
#409 opened - 0
Definition of String Vector
#408 opened - 0
Extend Aero Data Sets for Loads
#407 opened - 1
doorAssemblyPositionType
#406 opened - 2
mWindow
#405 opened - 1
Extend massBreakdown
#404 opened - 1
Fuselage tank definition
#403 opened - 1
Improve Rib Definition documentation
#402 opened - 2
Explicit stringer definition
#401 opened - 1
Wing stringer angle reference
#400 opened - 1
Trailing edge device wing cut out
#399 opened - 1
Explicit Rib Positioning
#398 opened - 1
Additional Rib Positioning
#397 opened - 1
Additional Spar Positioning
#396 opened - 1
Center Wing Box Top Decker
#395 opened - 0
Symmetry definition
#394 opened - 0
Dokumentaiton of profile definition
#393 opened - 0
Structural profile documentation
#392 opened - 0
CutOutProfile should not be mandatory
#391 opened - 1
Add Flight Dynamics
#390 opened - 1
Add Flight Performance
#389 opened - 1
Add Flying Qualities
#388 opened - 2
Toolspecifics Mapet
#387 opened - 1
Toolspecifics Harem
#386 opened - 4
LoadCases
#385 opened - 0
Design mass breakdown
#384 opened - 1
- 2
Include DELiS toolspecific
#382 opened - 1
- 2
Additional geometric entities
#380 opened - 3
New Guidecurves
#379 opened - 1
- 4
Profile Definition Thick Trailing Edge
#377 opened - 1
Upper and Lower Cap for Ribs
#376 opened - 2
Stringers in Cells should be optional
#375 opened - 4
Projection for ComponentSegments
#374 opened - 2
- 2
Flight Plan Proposal
#372 opened - 2
Systems Documentation
#371 opened - 5
Uncertainty in CPACS
#370 opened - 1
Fuselage symmetry in example file
#369 opened - 1
Cabin Items
#368 opened - 2
AeroPerformanceMap
#367 opened - 1
Leading, Trailing and Spoiler Type Sequence
#366 opened - 2
Cost assessment
#365 opened - 4
- 1
- 2
Split LE, TE and Spoiler
#362 opened