Repeat Example 5 .10 for the other two wings tested by Queijo et al. (1956) and compare

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Repeat Example 5 .10 for the other two wings tested by Queijo et al. (1956) and compare the VLM predictions to the experimental measurements.

Data from Example 5.10

Calculate the roll stability derivatives for a flat-plate wing with aspect ratio 6 and taper ratio 0.6 and compare to experimental measurements.

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