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Changelog

Version 0.7.4

Modified:

  • Added tuning factor for ratio between MLW and MZFW. (#51)

Version 0.7.3

Modified:

  • Added scaling factors for tuning HTP and VTP areas. (#49)

Version 0.7.2

Modified:

  • Python 3.12 is now supported. (#48)
  • Python 3.8, that reached end of life, is no longer supported. (#48)

Version 0.7.1

Fixed:

  • Incorrect comments in a datafile for CeRAS notebook would cause crash with FAST-OAD-core 1.8+. (#47)

Version 0.7.0

Fixed:

  • Fixed tail geometry (Warning: slight but noticeable changes in tail CG, hence in overall data). (#45)

Version 0.6.1

Added:

  • Compatibility with Python 3.11. (#43)

Version 0.6.0

Changed:

  • More control on calculation of load factors. (#38)
  • Update on geometry of tail planes (#36)

Fixed:

  • Restored the default solver behaviors of v0.4 for models with inner loop. (#39)

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