I need a report about aerodynamics characteristics of a two dimensional NACA 23012 aerofoil with a 20% scaled NACA 23012 plain flap. the aerofoil will be modelled at 0 degree angle of attack with falp settings of 0,10,20,30,40 degrees. reynold number of 1400000 to study the turbulent characteristics of the combo. the lift and drag coefficient and flow seperation will be determined using standard, RNG k-e and realizable k-e tuebulence models to assess the most appropriate model to be applied.
https://highmarkwriters.com/wp-content/uploads/2021/08/higmarklogo-300x60.png 0 0 pkariuki https://highmarkwriters.com/wp-content/uploads/2021/08/higmarklogo-300x60.png pkariuki2023-01-17 21:22:012023-01-17 21:22:12I Need A Report About Aerodynamics Characteristics Of A Two Dimensional Naca 23012 A 2838809
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