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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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Duct With Flow Control-Aircraft maintenance: BERNOULLI'S THEOREM This theorem can be related to the relationship between pressure and velocity existing in the air flowing
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The Mode II fracture toughness is measured using the ENF Typically, the specimen length is 120 mm, the width B is 20 mm, the thickness is between 3 and 5 mm and the distance be
ADVANTAGES The small size of the IC is its most apparent advantage. A typical IC can be constructed on a piece of semiconductor material that is less than 4mm2. Even when the
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original temp. of plate is 25 degree c.when put in burnace its upper part is 250 c and lower is 100 and mass is 56kg.find out heat transfer
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