Question: If I want to locate my minimum pressure at 0.5 of chord c then ___
Options
A : NACA 6512
B : NACA 652132
C : NACA 65211
D : NACA 0009
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Airfoil Selection-3 more questions
A NACA 22104 airfoil is operating at AOA = 3?.....
An airfoil is operated with flow velocity such that the....
An airfoil is such that the drag produced by airfoil....
Determine the corrections or otherwise of the following assertion [A]....
Laminar bucket is region where __
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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