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13-03-2024
Engineering

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In studying the aerodynamic impact of leading and trailing edge flaps on an airfoil, the camberline is considered. What is the camberline illustrated in?
a) y = x² - 3x + 2
b) y = 2x² - 6x + 4
c) y = 3x² - 9x + 6
d) y = 4x² - 12x + 8

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