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Calculate the pressure coefficient at a point on the airfoil where the pressure is \( 8.9 \times 10^4\,N/m^2\). Airfoil is …
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Calculate the lift, drag and moment coefficient about quarter chord per unit span of an airfoil which is at an …
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What are angle of attack, absolute angle of attack and induced angle of attack?
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What is center of pressure and aerodynamic center?
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Why induced drag is minimum for an elliptical wing planform?
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What are neutral point and static margin of an aircraft?
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What are longitudinal static stability, directional static stability and lateral static stability for an airplane?
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What is the difference between symmetrical and asymmetrical /cambered airfoil?
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Define airfoil terminology and NACA series of airfoil nomenclature.
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What is Bernoulli’s theorem?
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