Question Tag: lift
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A NACA 0012 airfoil having a chord of \(2.3\,m\) is in an airstream velocity of \(70\,m/s\) at standard sea level …
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A positively cambered airfoil has a zero-lift angle of \(-3.5^{\circ}\). The lift slope for this airfoil is \(0.12\) per degree. …
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Find the circulation around a spinning circular cylinder in free stream flow of velocity \(40\,m/s\) at a standard sea level …
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What are angle of attack, absolute angle of attack and induced angle of attack?
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What is the difference between symmetrical and asymmetrical /cambered airfoil?
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What is Bernoulli’s theorem?
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What are lift and drag forces in aircraft?
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