Problem (2): (18 points) A symmetric airfoil has a trailing edge flap which is 25% of chord in length and is deflected b

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Problem (2): (18 points) A symmetric airfoil has a trailing edge flap which is 25% of chord in length and is deflected b

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Problem 2 18 Points A Symmetric Airfoil Has A Trailing Edge Flap Which Is 25 Of Chord In Length And Is Deflected B 1
Problem 2 18 Points A Symmetric Airfoil Has A Trailing Edge Flap Which Is 25 Of Chord In Length And Is Deflected B 1 (166.52 KiB) Viewed 14 times
Problem (2): (18 points) A symmetric airfoil has a trailing edge flap which is 25% of chord in length and is deflected by 15 degrees. Use thin airfoil theory to find the lift coefficient of this airfoil when it is at 4 degrees angle of attack. 4 deg 15 deg VO dz dx foro s50.75 for 0.75 s.si -atan(159)
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