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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
Low pressure turbine clearance control valve: At take-off and low altitude the valve is in its normal closed position allowing cooling airflow to the core compartment. When an
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simplify using k-map f=sum(0,4,5,6,9,10,12)+d(1,15)
Fuel control system in Aircraft Engine: The computer controls the fuel flow to the engine to maintain a constant rotor RPM. During normal operation the optimum engine/rotor spe
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a part of machine has a reciprocating motion which is simple harmonic making 200 complete oscillations in a minute.the part weight 45 N.determine the accelerating force upon it
Bay cooling in Aircraft: There are two methods of bay cooling, they are: • Ram air cooling • Fan air cooling RAM AIR COOLING For ram air cooling, the aircraft has to
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