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AoA derivative for NACA0012?

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Old   April 15, 2016, 13:53
Default AoA derivative for NACA0012?
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Ryan Barrett
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I want to find the adjoint derivative of drag with respect to AoA for the NACA0012. I found the Sens_AoA in the history.csv file when I run the ADJOINT using the QuickStart files. But when I do finite difference this value is not even close to what the finite differences says the derivative should be. Is this the way to get the AoA derivative or is there a better way? There are lots of design variables available but I can't figure out a way to get the derivative of angle of attack.

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Old   April 22, 2016, 03:15
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Francisco Palacios
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Hi,
I'm using the sensitivity with respect to the AoA and the error compared with FD is acceptable. Are you sure that you are using 1/rads or 1/deg in both numbers? as you know, the factor is 57.2957795131. as far I remember Sens_AoA uses 1/rads

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Francisco Palacios
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Old   April 28, 2016, 17:57
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Ryan Barrett
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That did the trick. I thought it was in 1/deg not 1/rad. Thanks!
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