Topic: "vortex-panel-method"
Applied-Scientific-Research/Omega2D
Two-dimensional flow solver with GUI using vortex particle and boundary element methods
Language: C++ - Size: 16.8 MB - Last synced at: 11 months ago - Pushed at: about 2 years ago - Stars: 28 - Forks: 5
coding4Acause/PANKH
PANKH (Panel Analysis of uNsteady Kinematics of Hovering airfoils) is a solver for studying unsteady aerodynamics of flapping and hovering airfoils using the unsteady vortex panel method. This repository includes the source code, example cases, and validation results.
Language: C++ - Size: 28 MB - Last synced at: 2 months ago - Pushed at: 2 months ago - Stars: 1 - Forks: 0
asbhanarkar/Drag-estimation
The main objective of this project is to create a MATLAB code using Vortex Panel Method to compute pressure coefficient, tangential velocity and aerodynamic forces of given object.
Size: 31.3 KB - Last synced at: over 1 year ago - Pushed at: over 3 years ago - Stars: 1 - Forks: 0
Eliasfarah0/Vortex-Panel-Method-for-Airfoil-Aerodynamic-Coefficients
This repository makes use of the Vortex Panel Method to calculate the Lift, Drag and Pressure Coefficients of any airfoil at a specified Freestream Velocity, Chord Length and Angle of Attack by providing the X and Y coordinates of the airfoil in a .dat file.
Language: MATLAB - Size: 7.81 KB - Last synced at: over 1 year ago - Pushed at: almost 4 years ago - Stars: 0 - Forks: 1
