Repeat Example 4 .8 with increasing amounts of camber. Is there a visible change in the frequency

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Repeat Example 4 .8 with increasing amounts of camber. Is there a visible change in the frequency responses of the unsteady aerodynamic loads?

Data from Example 4.8

Calculate the aerodynamic loads acting on a sinusoidally pitching and plunging flat plate using the frequency domain version of the lumped vortex method. Compare the resulting aerodynamic load predictions to those of Theodorsen theory.

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