Question: Laminar bucket is region where __
Options
A : flow remains laminar
B : turbulent is produced
C : drag increases drastically
D : lift is reduced drastically
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Let's consider we need to design supersonic aircraft then, which....
Location of aerodynamic centre for low speed airfoil is __
The maximum lift co-efficient for NACA 19584 (chord=2.5m) airfoil is__
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What will be the location of maximum camber for NACA....
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