10.00pt/s C x2 + 2y - 8 =0 1.) x2 + 6y = 5 Calculate the lift...

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10.00pt/s C x2 + 2y - 8 =0 1.) x2 + 6y = 5 Calculate the lift and drag of the wing (full span) shown below (half span) if it is flying at 25000 ft. With an airsp eed of 260 ft/s. Let Cl = 0.98 and Cd = 0.064. (answer should be in English) Enter your

Posted Date: Jun 26, 2024 02:11 PM

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10.00pt/s C x2 + 2y - 8 =0 1.) x2 + 6y = 5 Calculate the lift...

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