v0.2.0

0.2.0 (2023-02-21)

Features

• Add new system Atmosphere and TurbofanWithAtm to ease computing of ambient conditions (from altitude, Mach and delta tamb)
• Use pythermo for gas modeling

API

• Add Compressor to public API of the systems.compressor and systems modules

Bug fix

• Fix TurbineAero exit total pressure computation from polytropic efficiency
• Fix some descriptions, especially related to gas models
• Fix incorrectly automatic pulling of fan_duct_core_cowl_slope in Turbofan
• Fix demo turbofan notebook to set design targets before adding targets to the non-linear solver

v0.1.0

0.1.0 (2022-10-18)

Features

• Add additional models
  • add assemblies: Turbofan, FanModule, Inlet, MixerFluid/MixerShaft, Nacelle, Nozzle, Channel
  • add various standalone and base models: FanDuctGeom, TurbofanGeom, etc.
• Improve gas thermodynamic modeling (IdealGas)

Code quality & packaging

• Add documentation using sphinx (incl. demo notebook rendering using nbsphinx)
• Improve code quality using black, isosort and flake8
• Improve tests coverage

v0.0.1

0.0.1 (2022-05-25)

Features

• First release
  • base models added: compressor, turbine, combustor, etc.
  • systems/assemblies added: fan module, gas generator, etc.

Code quality & packaging

• Package structure (license file, etc.)
• Tests using pytest