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Is 17% is the thickness of NASA LS-0417 airfoil?

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Is 17% is the thickness of NASA LS-0417 airfoil?

(a) True

(b) False

This question was posed to me in an online quiz.

My question is based upon Modern Low Speed Airfoils in division Incompressible Flow over Airfoils of Aerodynamics

1 Answer

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by (720k points)
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The correct option is (a) True

Explanation: The NASA LS- 0417 airfoil has a maximum thickness of 17% and a design lift coefficient of 0.4. Using the same camber line, NASA has extended this airfoil into a family of a low-speed airfoil of different thickness for example LS-0409 and the LS-0413.

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