I want a general idea of how much thrust an airfoil will produce at a set speed with a set shape
I would also like to know how much resistance it has in a set density gas
I know the math exists for liquids but wikipedia say that for gasses the math is to long and it thusly isn't shown there
I can understand why its a long bit of math but i just need an approximate answer even if the error puts it off by 30%
I would also like to know how much resistance it has in a set density gas
I know the math exists for liquids but wikipedia say that for gasses the math is to long and it thusly isn't shown there
I can understand why its a long bit of math but i just need an approximate answer even if the error puts it off by 30%
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