Question: So what sweep angle would be better for an oblique - wing aircraft where it pivots the wing to go supersonic? We are planning on

So what sweep angle would be better for an oblique

-

wing aircraft where it pivots the wing to go supersonic?

We are planning on a project to creating a design of an airliner with oblique wing along with additional compression lift device where the design will include measurements of the Concorde.

Here it was mentioned that sweeping from

45

degrees is risky to handle

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