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GATE 2021 AE – Question 25

Aerodynamics · Airfoils and wings: coefficients, Kutta-Joukowski theorem, thin airfoil theory, finite wing theory, critical and drag divergence Mach numbers · 1 mark · Multiple select

Which statements about the Kutta condition are correct?

  1. It determines circulation around an airfoil.
  2. It applies to airfoils with a sharp trailing edge.
  3. The trailing edge must always be a stagnation point.
  4. The flow leaves the trailing edge smoothly.

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Show answer and explanation

Correct answer: (A) It determines circulation around an airfoil.; (B) It applies to airfoils with a sharp trailing edge.; (D) The flow leaves the trailing edge smoothly.

Explanation

The **Kutta condition** fixes the circulation around a lifting airfoil in potential flow.

Answer **A, B and D**.