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Is it possible to manipulate AAA to analyze a blended wing-body (BWB) airplane configuration?

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Is it possible to manipulate AAA to analyze a blended wing-body (BWB) airplane configuration?

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You can define a flying wing by indicating there is no horizontal, no V-Tail, no canard and no vertical tail. You can supply fuselage parameters for the part of the blended body that is used as fuselage. We do not have a trim module for flying wings. Weights and S&C derivatives can be used for flying wings.

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