Alexander Giles
University of Strathclyde
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Inviato
Simple unsteady vortex code to demonstrate wake rollup
2D unsteady aerodynamic code in which the aerofoil is represented by a single vortex
quasi 11 anni fa | 4 download |
Inviato
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
quasi 11 anni fa | 2 download |
Inviato
Panel method for the simulation of the performance of a biplane
Doublet and source formulation (Dirichlet boundary condition)
quasi 11 anni fa | 3 download |
Inviato
Panel method for NACA XXXX aerofoils
Panel method using doublets and sources with the Dirichlet boundary condition
quasi 11 anni fa | 1 download |
Domanda
Problem with Simulink Model
Hello, I am currently investigating the behaviour of a distributed generator following an islanding event (loss-of-mains). I ...
circa 13 anni fa | 1 risposta | 0



