Changelog

Version 0.5.0

Changed:

• Allowing deactivation of inner solvers. (#33)

• Having ISA temperature offset as input of engine deck. (#31)

Version 0.4.0

Changed:

• FAST-OAD-CS25 is now officially compatible with Python 3.10. Support of Python 3.7 has been abandoned. (#26)

• Trailing edge of wing inner part can now have a non-zero sweep angle.(#27)

• Now the criteria for computation of wing can be controlled through options. (#29)

• Computation of wing geometry now uses sub-models and has now an option for (de)activating the computation of wing thickness. (#29)

Fixed: - Fixed component for computing global positions of wing chords, which is now a sub-model of geometry module (#28)

Version 0.3.0

Changed:

• OpenMDAO 3.18+ is now required. (#18)

• Submodels have been introduced in module “fastoad.loop.wing_area”. (#7)

• Load factors are now explicitly in output data. (#23)

Fixed:

• Unit of variable “data:weight:aircraft:additional_fuel_capacity” has been corrected to “kg”. (#18)

• Unit of “*:CL_alpha” variables is now consistently “1/rad”. (#21)

• Unit for “data:load_case:lc2:Vc_EAS” has been corrected to “m/s”. (#23)

Version 0.2.0

Added:

• Now polar computation in aerodynamics module computes angle of attack as a linear function of CL. (#16)

Version 0.1.4

Fixed:

• Bundled notebooks have been modified to adapt to FAST-OAD 1.4.1, which is now the minimum required version for FAST-OAD-core. (#14)

Version 0.1.3

Fixed:

• in bundled notebooks:

  • Generation of configuration file would fail if several FAST-OAD plugins were installed.

  • Link to CeRAS website has been fixed

Version 0.1.2

Changed:

• Now allowing wing geometry with no kink (#3)

Fixed:

• Fixed deprecation warnings (#4)

• Now allowing versions greater than 0.1 for StdAtm

Version 0.1.1

• Fixed dependency to FAST-OAD

Version 0.1.0

• FAST-OAD CS-25 related models are now in this separate package