Aerospace Engineering > GATE 2016 > Airfoil Geometry
Which of the following airfoil will have location of the maximum camber at half chord length from the leading edge?
A
NACA 5212
B
NACA 1225
C
NACA 2215
D
NACA 2512

Correct : d

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Related Topics

NACA airfoil maximum camber location half chord length NACA designation Aerospace Engineering GATE 2016 airfoil properties GATE Aerospace Engineering NACA 2512

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