(Solved): (b) A NACA 6412 aerofoil is shown in the figure below Figure Q1b not to scale Assuming an airc ...

(b) A NACA 6412 aerofoil is shown in the figure below Figure Q1b – not to scale Assuming an aircraft using a NACA 6412 geometry has a wing chord of 3.25m, determine; (i) The maximum camber [1] (ii) The position of maximum camber relative to the leading edge [1] (iii) The maximum thickness [1] (iv) The camber value 1m from the leading edge [3] (b) A NACA 6412 aerofoil is shown in the figure below Figure Q1b – not to scale Assuming an aircraft using a NACA 6412 geometry has a wing chord of 3.25m, determine; (i) The maximum camber [1] (ii) The position of maximum camber relative to the leading edge [1] (iii) The maximum thickness [1] (iv) The camber value 1m from the leading edge [3]