Question: Let's consider we need to design supersonic aircraft then, which type of airfoil should be adopted?

Options

A : Supersonic airfoil

B : Symmetric airfoil

C : Bluff shape

D : Thicker airfoil

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Airfoil Selection-3 more questions

Determine the corrections or otherwise of the following assertion [A]....

Fuel system includes __

If I want to locate my minimum pressure at 0.5....

Integral tanks are ___

Laminar bucket is region where __

Location of aerodynamic centre for low speed airfoil is __

The maximum lift co-efficient for NACA 19584 (chord=2.5m) airfoil is__

What is the disadvantage of bladder fuel tank?

What will be the location of maximum camber for NACA....

Which of the following is not the type of fuel....

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