Calculation of Lift/Drag ratio #181
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DinoBird25
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Hi @DinoBird25, please see the sample here: #16 (comment) Kind regards, |
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I was working on the concorde sample setup with a custom made model. I wish to find the Lift/Drag ratios for research purposes, I tried to implement the existing guidance on the forum but it ended up getting zero values. Does anyone have a sample setup of an aircraft where they get a report of lift/drag ratio. Thank you for help.
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