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Is practical use twist (geometric or multiple airfoils to improve stall characteristics) when it has lift coefficient distribution ideal or near due to wing plataform?

I am analyzing a "Schuemann" wing, and I am in the dilemma of whether to use a twist (multiple airfoils or geometrical) to improve stall and look for compromise or investigate other forms directly (vortex generator, e.g.).

Is to a Sailplane project

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  • $\begingroup$ What do you mean with improve stall characteristics? An higher max AoA? A milder stall? An earlier stall warming? $\endgroup$
    – sophit
    Nov 5, 2023 at 11:29
  • $\begingroup$ Stall warning. I chose the airfoil with higher max AOA and docile stall. Thanks $\endgroup$
    – andy
    Nov 5, 2023 at 15:57
  • $\begingroup$ @andy What type of ship is this...a sailplane?? powered aircraft? Is this full scale, or RC? $\endgroup$ Nov 8, 2023 at 21:44

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