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Hi, I have read your work and from the article I read that you assumed an incompressible flow (M= 0.1-0.3). In your opinion could I train the ANN for a wider range of fligh conditions?
The text was updated successfully, but these errors were encountered:
Hello @sarapuccia. Ideally, yes you can train a similar architecture for a wider range of flight conditions provided you've enough training dataset to capture variations across a supersonic flow.
Hi, I have read your work and from the article I read that you assumed an incompressible flow (M= 0.1-0.3). In your opinion could I train the ANN for a wider range of fligh conditions?
The text was updated successfully, but these errors were encountered: