CPACS 3.0

  • New component segment definition; this is affecting all structural components of wings
  • Renamed angleOfYaw into angleOfSideslip
  • Fixes in documentation
  • Made all uID attributes required
  • Minor fixes in choices & typos
  • Added nodes for the geometry of generic system components
  • Added performance requirements for aircraft models
  • Redefined the whole mission definition including point performances
  • Made link to missionUID in trajectory optional
  • Added new parameters to enginePerformanceMap
  • Relocated mFixedLeadingEdge and mFixedTrailingEdge within the massBReakdown structure
  • Changed aeroPerformanceMap to use altitude and standard atmosphere instead of reynolds number
  • Added an optional local direction for guide curves and an illustrational image
  • Announced toolspecifcs definitions as depricated; will be removed from CPACS in next release and should be managed in separate namespace by tool maintainers
  • Added an option for aerodynamic performance maps of elastic aircraft
  • Enabled the definition of multiple aeroPerformanceMaps
  • Enabled the use of spar points for rib placement and rib points for spar placement
  • Added explicit stringer definitions for wing cells

All issues for this release can be found online
https://github.com/DLR-LY/CPACS/issues

Assets 3

@DLR-LY DLR-LY released this Jul 29, 2016 · 125 commits to master since this release

CPACS 2.3.1

  • Added a branch for the definition of design studies.
  • Added thermal properties for materials.
  • Revised the definition of flights/flightplans.
  • Added an airline definition.
  • Added structure for skid gear components.
  • Changed the units for material density to SI units.
  • Revised the top level fleets node and put it into the new airline node.

All issues for this release can be found online
https://github.com/DLR-LY/CPACS/issues

Assets 4
Jul 29, 2016
Added release statement and changed version number and date.

@boeh-da boeh-da released this Nov 4, 2015

CPACS 2.3 release is now available

  • Included vector notation for weight and balance.
  • Included flight system and flight dynamic information.
  • Included top level aircraft requirements.
  • Included a prototype for detailed nacelle geometries.
  • Included structural mounts.
  • Extended aero data set for loads.
  • Extended the mass breakdown.
  • Updated the symmetry definition, please take a look at the documentation point 5 adn 6.

All issues for this release can be found online
https://github.com/DLR-boeh-da/CPACS/issues?utf8=%E2%9C%93&q=+milestone%3A%22CPACS+2.3%22+

Assets 3