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engenuity - innovation through engineering analysis Non-dimensionalised Pressure DistributionPressure DistributionCp distribution

Analysis of 2D Aerofoil Section

1: Objectives
2: Case Conditions
3: Modelling
4: Case Set-Up
5: Results and Conclusions

To examine the aerodynamic characteristics of a two-dimensional aerofoil at a given Chord Reynolds Number and Mach Number.

In particular, to predict the angle of incidence at which the section will generate a Lift Coefficient of 0.5.

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