www.Airloads.net

 

Program Airloads-V4 :

An Object Oriented Symbolic Algorithm For Aero/Hydrodynamic Design And Simulation

 

Program Abilities :

1- Two Dimensional Geometry Package :

2- Two Dimensional Solvers :

  • Thin Airfoil Theory , concentrated trigonometric distribution of vortices along the camber line
  • Lumped Vortex panel method , concentrated lumped distribution of vortices at the quarter chord of each panel assembling the camber line
  • Constant Source + Constant Vortex Panel Method , surface distribution of constant sources and constant vortices at each panel assembling the surface , the sources are different for each panel but the vortex is the same
  • Linear Vortex Panel Method , surface distribution of linearly varying vortices distributed over each panel assembling the surface

3- Three Dimensional Geometry Package :

  • Frame by frame method
  • Rotate two different parametric numeric or symbolic curves in space to generate a body of revolution . Two curves to generate the upper and lower parts separately

4- Three Dimensional Solver :

5- Dynamics Simulation Package :

6- Tricks and Tweaks :

 

The program is a one man project started at 2008

 

Vortex Lattice Method

 

 

 

 

vortex lattice method

 

vortex lattice method

 

Vortex Lattice Method

 

 

 

 

 

Vortex Lattice Method

 

vortex lattice method

 

vortex lattice method

 

vortex lattice method

 

vortex lattice method

 

vortex lattice method

 

 

vortex lattice method

 

 

vortex lattice method

 

Vortex Lattice Method

 

Vortex Lattice Method

 

Vortex Lattice Method

 

 

 

 

 

 

 

 

 

 

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