This release overhauls the ADflow options (#102, #41), which may break existing run scripts in the following ways: 1) The options autosolveretry, autoadjointretry, and nkcfl0 are now deprecated. These options have had no function for years but may still be in old scripts. 2) String-type option values are now case sensitive and several of the acceptable string values have changed. This will most commonly affect equationType. For example, you must use "RANS" instead of "rans". Please refer to the options documentation for the acceptable values. The full list of affected string-type options is: solutionPrecision gridPrecision solutionPrecisionSurface gridPrecisionSurface discretization coarseDiscretization limiter smoother equationType equatio...
What's Changed Improved cavitation constraint by @yqliaohk in https://github.com/mdolab/adflow/pull...
New features Added an option to specify acceptable adjoint convergence (#168) Time spectral with fl...
ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization
This minor release has the following changes: Updated default options for testing (#128) Added an o...
This is patch release with the following changes: Bug fixes Fixed MExt (#138) Fixed option printin...
New features Dissipation-based continuation for flows with shocks by @sseraj in https://github.com/...
This release contains the following bug fixes: fixed updategamma() (#91) updated displacement file ...
New features Option to write solution files after every major iteration (#187) kwargs for addPointS...
This minor release has the following changes: Better support for running tests locally or Azure pip...
New features added rootSetOption and error estimation by @nwu63 in https://github.com/mdolab/adflow...
This release includes the following changes: Bugfix for turbulence advection order (#63) Documentat...
This release brings the following bugfixes: Copying spectral radii back to main memory after blocke...
This patch release contains the following changes: Various testing updates (#95) Adding information...
New features adding new mphys wrapper and removing the old openmdao wrappers by @anilyil in https:/...
This patch release includes the following change: self.comm is now set in baseSolver, argument list...
What's Changed Improved cavitation constraint by @yqliaohk in https://github.com/mdolab/adflow/pull...
New features Added an option to specify acceptable adjoint convergence (#168) Time spectral with fl...
ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization
This minor release has the following changes: Updated default options for testing (#128) Added an o...
This is patch release with the following changes: Bug fixes Fixed MExt (#138) Fixed option printin...
New features Dissipation-based continuation for flows with shocks by @sseraj in https://github.com/...
This release contains the following bug fixes: fixed updategamma() (#91) updated displacement file ...
New features Option to write solution files after every major iteration (#187) kwargs for addPointS...
This minor release has the following changes: Better support for running tests locally or Azure pip...
New features added rootSetOption and error estimation by @nwu63 in https://github.com/mdolab/adflow...
This release includes the following changes: Bugfix for turbulence advection order (#63) Documentat...
This release brings the following bugfixes: Copying spectral radii back to main memory after blocke...
This patch release contains the following changes: Various testing updates (#95) Adding information...
New features adding new mphys wrapper and removing the old openmdao wrappers by @anilyil in https:/...
This patch release includes the following change: self.comm is now set in baseSolver, argument list...
What's Changed Improved cavitation constraint by @yqliaohk in https://github.com/mdolab/adflow/pull...
New features Added an option to specify acceptable adjoint convergence (#168) Time spectral with fl...
ADflow is a finite volume RANS solver tailored for gradient-based aerodynamic design optimization