KlausG

Thanks, Stefan! At the moment I take the average CL over the span and insert it into the Lift-formula (CL * ro/2 * A * v2). I just wondered, because alle the values are there, would be easy to implement it! By the way, for my planned aluminium-fuselage I have safety factor 1,5. But you never kow :-) regards, Klaus

Short version: For a defined plane: Where can I see the total lift (in Newton) separately for main wing and elevator for different OP-Points?

Maybe a stupid question and/or often asked, but I could not find an answer in this forum: My hydrofoil consists of Mainwing and Elevator. Analysis with fixed lift, because the lift of the complete plane must always compensate the weight of board+rider. For all Wingfoil-hydrofoils the elevator is mounted "upside down" and therefore generating negative lift for nearly all Op-Points. The lower the AOA of the mainwing, the higher the AOA of the upsidedown-mounted-elevator: The lower the AOA of the mainwing...

Maybe a stupid question and/or often asked, but I could not find an answer in this forum: My hydrofoil consists of Mainwing and Elevator. Analysis with fixed lift, because the lift of the complete plane must always compensate the weight of board+rider. For all Wingfoil-hydrofoils the elevator is mounted "upside down" and therefore generating negative lift for nearly all Op-Points. The lower the AOA of the mainwing, the higher the AOA of the upsidedown-elvator and the more downward lift is generated...

Maybe a stupid question and/or often asked, but I could not find an answer in this forum: My hydrofoil consists of Mainwing and Elevator. Analysis with fixed lift, because the lift of the complete plane must always compensate the weight of board+rider. For all Wingfoil-hydrofoils the elevator is mounted "upside down" and therefore generating negative lift for nearly all Op-Points. The lower the AOA of the mainwing, the higher the AOA of the upsidedown-elvator and the more downward lift is generated...

Maybe a stupid question and/or often asked, but I could not find an answer in this forum: My hydrofoil consists of Mainwing and Elevator. Analysis with fixed lift, because the lift of the complete plane must always compensate the weight of board+rider. For all Wingfoil-hydrofoils the elevator is mounted "upside down" and therefore generating negative lift for nearly all Op-Points. The lower the AOA of the mainwing, the higher the AOA of the upsidedown-elvator and the more downward lift is generated...

Maybe a stupid question and/or often asked, but I could not find an answer in this forum: My hydrofoil consists of Mainwing and Elevator. Analysis with fixed lift, because the lift of the complete plane must always compensate the weight of board+rider. For all Wingfoil-hydrofoils the elevator is mounted "upside down" and therefore generating negative lift for nearly all Op-Points. The lower the AOA of the mainwing, the higher the AOA of the upsidedown-elvator and the more downward lift is generated...

Maybe a stupid question and/or often asked, but I could not find an answer in this forum: My hydrofoil consists of Mainwing and Elevator. Analysis with fixed lift, because the lift of the complete plane must always compensate the weight of board+rider. For all Wingfoil-hydrofoils the elevator is mounted "upside down" and therefore generating negative lift for nearly all Op-Points. The lower the AOA of the mainwing, the higher the AOA of the upsidedown-elvator and the more downward lift is generated...