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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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Trim tabs are small flaps attached to the rear of the main control surfaces. They can be adjusted the pilot to reduce the force required to hold the control surface in its deflecte
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