Gallery#
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Aero-propulsive analysis of an optimized multi-element airfoil# |
Optimization using XFOIL (10x speed)# |
XFOIL analysis of the NACA 0012 airfoil at \(M=0.1\) and \(\alpha=\{0^\circ,1^\circ,2^\circ\}\)# |
MSES analysis of the NASA SC20612 airfoil at \(M=0.67\) and \(\alpha=\{0^\circ,1^\circ\}\)# |
Modification of design variables# |
Plotting aerodynamic field variables# |
Polar analysis workflow for a custom airfoil# |
Aerodynamic polars for a custom airfoil# |
Matching a NASA SC20612 airfoil with Bézier curves (4x speed)# |
Customization of the GUI# |
Aero-propulsive analysis of an optimized multi-element airfoil# |
Optimization using XFOIL (10x speed)# |
XFOIL analysis of the NACA 0012 airfoil at \(M=0.1\) and \(\alpha=\{0^\circ,1^\circ,2^\circ\}\)# |
MSES analysis of the NASA SC20612 airfoil at \(M=0.67\) and \(\alpha=\{0^\circ,1^\circ\}\)# |
Modification of design variables# |
Plotting aerodynamic field variables# |
Polar analysis workflow for a custom airfoil# |
Aerodynamic polars for a custom airfoil# |
Matching a NASA SC20612 airfoil with Bézier curves (4x speed)# |
Customization of the GUI# |