GATE AE · 2026 · AE
Question 63: Airfoils and Wings
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Question 63
AENAT2 marksNeeds review
Thin airfoil theory predicts the zero-lift angle of attack
of NACA 2412 airfoil as
. The corresponding prediction of
for NACA 5410 airfoil is ________ degrees (rounded off to 1 decimal place).Log in to check the answer
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2026AE
GATE AE 2026 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Numerical answer (NAT)
- Marks
- 2 marks
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