Alexander Giles
University of Strathclyde
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Simple unsteady vortex code to demonstrate wake rollup
2D unsteady aerodynamic code in which the aerofoil is represented by a single vortex
10년 초과 전 | 다운로드 수: 9 |
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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
10년 초과 전 | 다운로드 수: 2 |
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Panel method for the simulation of the performance of a biplane
Doublet and source formulation (Dirichlet boundary condition)
10년 초과 전 | 다운로드 수: 1 |
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Panel method for NACA XXXX aerofoils
Panel method using doublets and sources with the Dirichlet boundary condition
10년 초과 전 | 다운로드 수: 11 |
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Problem with Simulink Model
Hello, I am currently investigating the behaviour of a distributed generator following an islanding event (loss-of-mains). I ...
12년 초과 전 | 답변 수: 1 | 0



