Alexander Giles
University of Strathclyde
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Feeds
Submitted
Simple unsteady vortex code to demonstrate wake rollup
2D unsteady aerodynamic code in which the aerofoil is represented by a single vortex
10 years ago | 6 downloads |
Submitted
Simple panel method model for evaluating pressure distribution over symmetric NACA aerofoils
Constant strength doublet panel method for evaluating pressure distribution for symmetric NACA foils
10 years ago | 3 downloads |
Submitted
Panel method for the simulation of the performance of a biplane
Doublet and source formulation (Dirichlet boundary condition)
10 years ago | 1 download |
Submitted
Panel method for NACA XXXX aerofoils
Panel method using doublets and sources with the Dirichlet boundary condition
10 years ago | 13 downloads |
