Airfoils and lift compared to air density and TE
I am studing a flare system with compbustion and high speed flow using CFD simulation. I would like to compared the flow in the vicinity of the flare plume to data regarding the stability of an airfoil.
That means I am looking for what range is a generel airfoil of a airplane (small airplane) stabel.
Like a minimum limite of the air density ?
And what levels should the turbulence kinetic energy be below ?
Does anyone knows were to find such information ???
Thanks on advance.
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