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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
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I need help for my project report plz. > Precast concrete panels manufactured in factory environments and rapidly cured using steam are being used for the walls of shallow foundati
Noise reduction The problem of engine noise has always been associated with aircraft. Increases in engine power have given rise to increases in noise and the indications are t
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USE OF MULTICYLINDER ENGINE If, in a multi cylinder engine, power strokes are staggered, the limitation of flywheel can be overcome to a large extent. Torque diagram for 2 cyli
Propeller control : CONSTANT SPEED UNIT: In the normal flight range, the main control of the propeller is exercised by the propeller control unit (PCU). MANUAL AND AU
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