Repeat Example 5 .4 using the SDPM and compare the resulting pressure distributions to the experimental pressures

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Repeat Example 5 .4 using the SDPM and compare the resulting pressure distributions to the experimental pressures given in Kolbe and Boltz (1951).

Data from Example 5.4

Use the VLM to calculate the aerodynamic loads acting on a swept wing at several angles of attack and compare to experimental data.

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