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Design Features of Supercritical Aerofoil
• Blunt nose-
rapid p pressure reduction around leading edge
• Flat top-
Reduce the flow acceleration on upper surface toreduce shock strength
• Cusped trailing edge-
Increased loading over rear of aerofoil to recoversome lift
Velocity vector
Speed of NACA
floor
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Oil supply failure - Propeller: To prevent an overspeed caused by an oil supply failure, one of two methods may be employed: • Hydraulic lock valve The pitch lock mecha
serislization
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