From f83dc05bdc887324eed52fcba0acd98a19aa30f5 Mon Sep 17 00:00:00 2001 From: Jonas Jepsen Date: Tue, 31 Jul 2018 16:55:19 +0200 Subject: [PATCH] Added section for CPACS 3.0 release --- schema/cpacs_schema.xsd | 28 ++++++++++++++++++++++++++++ 1 file changed, 28 insertions(+) diff --git a/schema/cpacs_schema.xsd b/schema/cpacs_schema.xsd index a8c593d..76308ef 100644 --- a/schema/cpacs_schema.xsd +++ b/schema/cpacs_schema.xsd @@ -385,6 +385,34 @@ jonas.jepsen@dlr.de The temperature offset changes only the density (following rho = p / Gas Constant / T) (and viscosity, of course) + + CPACS 3.0 + + Release in Jul 2018 + + 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 and 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 illustration image + Announced toolspecifics definitions as deprecated; 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 + + + CPACS 2.3.1