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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
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It is recommended that if possible you should buy a copy of this book. It will prove useful for the new fourth year configurational aerodynamics module also. Blackwells bookshop ha
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