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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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SUPERSONIC INTAKES At supersonic speeds, the pitot type of air intake is unsuitable due to the severity of shock waves which form and progressively reduce the intake efficiency
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Inspection Checklist: The following checklist is a starting point and it may be added to if subsequent inspections and debriefs indicate that this would be beneficial. It sh
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