Estimation of different drag components (profile drag and wave drag) for a transonic wing #137
NIVEDITAG373
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Using Aerosandbox and neural foil, I was trying to estimate profile drag and wave drag for a transonic wing. Please provide a method to model the drag components of a swept wing in transonic regime using aerosandbox. Also, Is a license required to access and operate the 'mses.py' in AeroSandbox?
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