Question Tag: lift force
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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 gliding distance of an aircraft flying at an altitude of 1500\,m with a maximum lift to drag ratio …
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Define airfoil terminology and NACA series of airfoil nomenclature.
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What is canard in an aircraft?
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What are lift and drag forces in aircraft?
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