Aerospace Engineering > GATE 2022 > Airfoil Nomenclature
NACA 2412 airfoil has _______.
A
4% maximum camber with respect to chord
B
maximum camber at 40% chord
C
12% maximum thickness to chord ratio
D
maximum camber at 20% chord

Correct : b,c

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Related Topics

NACA 2412 airfoil airfoil nomenclature maximum camber maximum thickness to chord ratio aerospace engineering GATE 2022 GATE 2022 Q26 aerodynamics airfoil NACA airfoil properties

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