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Source of drage
Total Drag on an aerofoil is called profile drag
- Skin friction
• due to tangential force arising from friction
- Pressure
• Form - due to the integrated effect of pressuremodification from presence of the boundary layer
• Wave - due to the presence of shock waves
• The potential prediction of drag is zero- Inviscid, incompressible, irrotational
This is an individual task in the form of an essay of between 900 and 1300 words. Illustrative material such as pictures may be included in addition to the text.
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