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GATE 2022 AE – Question 26

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

NACA 2412 airfoil has

  1. 4% maximum camber with respect to chord
  2. maximum camber at 40% chord
  3. 12% maximum thickness to chord ratio
  4. maximum camber at 20% chord

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Show answer and explanation

Correct answer: (B) maximum camber at 40% chord; (C) 12% maximum thickness to chord ratio

Explanation

The **NACA 4-digit** series describes an airfoil by three numbers, for example 2412:

Check the options:
- A, 4% maximum camber: ✗ (it is 2%)
- B, maximum camber at 40% chord: ✓
- C, 12% thickness: ✓
- D, maximum camber at 20% chord: ✗

Answer **B and C**.