Question Tag: airfoil
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Starting with the definition of circulation, derive Kelvin’s circulation theorem.
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Consider an NACA \(2412\) airfoil with a \(2\;m\) chord in an airstream with a velocity of \(50\; m/s\) at standard …
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Consider the data for the NACA \(2412\) airfoil. Calculate the lift and moment about the quarter chord (per unit span) …
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The critical Mach number of an airfoil is attained when
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For a symmetric airfoil,the lift coefficient for zero degree angle of attack is
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