PaMS Panel Method Solver
 
 
VALIDATION TEST CASES
 
     
 
Cylinder: 2D steady - thick non-lifting bodies.  
Sphere: 3D steady - thick non-lifting bodies with both quadrilateral and triangular mesh.
NACA0012 airfoil: 2D steady - “Dirichlet” boundary condition for thick lifting airfoils.  
NACA63 mean line: 2D steady - “Neumann” boundary condition for thin lifting airfoil.
Elliptic wing: 3D steady - lifting wing.  
Oscillating flatplate: 2D unsteady - oscillating thin lifting airfoil.
Oscillating airfoil: 2D unsteady - oscillating thick lifting airfoil and aerodynamic interference.  
Rotor hovering: 3D unsteady - wake models at static thrust conditions.
Vertical Axis Wind Turbine: 3D unsteady - lifting wing and wake-body interaction.  
NASA SR-2 wing-prop: 3D unsteady - lifting wing and wake-body interference.
Tiltrotor: 3D unsteady - wing-propeller configuration @ angle of attack up to 90deg.  
Light aircraft: 3D steady - wing-fuselage configuration.
Internal flow: 3D steady - pipe.  
Helicopter: 3D unsteady - aerodynamic interaction between a helicopter rotor and an airframe.
Hi Lift PW-1: 3D steady - 1st AIAA Hi Lift Prediction Workshop.  
Hi Lift PW-2: 3D steady - 2nd AIAA Hi Lift Prediction Workshop.
 
 
     
             
by Paolo Caccavale