5. Splining and Refining Airfoil Contours — PyAero v'2.1.6
5. Splining and Refining Airfoil Contours — PyAero v'2.1.6' documentation
Pressure contours of flow over NPU-LSC-72613 airfoil at free transition.
13: Instantaneous Mach contours for the RAE2822 airfoil. Self-sustained
Comparison and Analysis of Natural Laminar Flow Airfoil Shape Optimization Results at Transonic Regime with Bumps and Trailing Edge Devices Solved by Pareto Games and EAs
Surface proximity flapped 3d lifting foil analysis
Constrained shape design of a transonic turbulent airfoil at a cte. CL
3. User Interface — PyAero v'2.1.6' documentation
PyAero documentation — PyAero v'2.1.6' documentation
Aeroacoustic airfoil shape optimization enhanced by autoencoders - ScienceDirect
Aeroacoustic airfoil shape optimization enhanced by autoencoders - ScienceDirect