v1.3.0

• Improvement of aerodynamic tools by @florentLutz and @johnathanasd
• Complete polar database by @florentLutz
• Optimization of turboprop model usage by @florentLutz
• Compatibility with Python 3.10 by @florentLutz

v1.2.2

• Update release process by @florentLutz

v1.2.1

• Now using Poetry 1.4.2 #205 by @florentLutz
• Allowing new version of stdatm #206 by @florentLutz. It is not made use of just yet in this repo
• Bug correction to allow compatibility with recent package update #211 by @florentLutz. Some features we used were not compatible with new package version so some slight changes were made.

v1.2.0

• Made use of the @functools.lru_cache function in order to save time on function that read .csv files see #188
• Reworked some of the solvers to save some time and deleted some that were not useful see #195
• Added yml as a viable input for the block analysis
• Development of high wing models by pulling the work of @fomra during his summer 2022 internship
• Implementation of twist and dihedral in logitudinal aerodynamics see #202
• Changed the function of the Cl=f(curve) to match a new reference wing Cl see #202

v1.1.0

• Modified the Xfoil interface to allow for single AoA launch see #182
• Modification of the usage of the FlightPoint dataclass so that it is possible to add new fields more easily see #187
• Added a module for the computation of more aerodynamic derivatives see #185

v1.0.4

• Added compressibility corrections and reynolds correction in the BEMT code
• Change in the propeller code organization
• Added a new representation of the propeller performance under the form of Ct and Cp graphs
• Centralized all post_processing function in a post-processing API
• Added an option for the path to airfoil files

v1.0.3

Removed unnecessary use of matplotlib in post_processing functions

v1.0.2

Updated binder requirements

v1.0.1

Changed the homepage address in the pyproject.toml

v1.0.0

• Added an analytical model for wing mass estimation
• Most models are now registered using the submodel feature from FAST-OAD-core
• Added an analytical model for fuselage mass estimation
• Dependencies were updated to reflected the separation between core and models in FAST-OAD
• Generalized the usage of shape_by_conn option when possible
• Added propeller installation effects
• Added link to Binder-hosted notebooks
• Sped up the computation of propeller performances, of aircraft performances and of IC engine fuel consumption
• Added a model for turboprop fuel consumption computation
• Added a new mission modules solves all the FlightPoints at once instead of using a time step approach
• Added Daher TBM900 as a reference aircraft