1. Panel method

This page shows the set of working examples using the panel method. These examples are all for the steady solver.

Examples 1 and 2 are demos for classic and well-known geometries.

• 1.1. NACA0012 rectangular wing
• 1.2. ONERA M6 case

Example 3 looks at a blended wing body configuration, modeling a series of cases across different angles of attack.

• 1.3. Blended wing body across many missions