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What is the flap adjustment angle for delta wing aircraft for take off for the Concorde and the SR-71 Blackbird, given that it has no horizontal stabilisers and that it used elevons?

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Concorde did not have any flaps or slats as mentioned here. This is due the fact that they don't have any tails, and wing trailing edge devices do the elevator and aileron jobs and they are called elevons.

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  • $\begingroup$ in essence only slats are adjusted $\endgroup$ Mar 11, 2018 at 12:04

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