Find the total lift coefficient for the wing given in Example 4 with i) theoretical approach, ii)

Question:

Find the total lift coefficient for the wing given in Example 4 with

i) theoretical approach, 

ii) with empirical correction.

Example 4

The wing given in Example 2 is undergoing a simple harmonic motion with \(h=\bar{h} e^{i \omega t}\). Find the lifting pressure on the wing surface in terms of the wing geometry and the reduced frequency.

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