- #1
Paradox101
- 47
- 1
Been working on a new way of determining the lift coefficient besides the thin airfoil theory,and I don't know if there is already such a method or if I'm wrong.Plz Help.We know,
L=CL×1/2ρv^2A
Now,as lift is a force,then it should be as L=mμ, where μ is the "upwards acceleration".
So, L=mμ=CL×1/2ρv^2A
⇒mμ=CL×1/2ρ[(0)^2+2as]A, because v^2=u^2+2as,and here the initial velocity will be zero.
⇒mμ=CL×1/2ρ2asA
⇒mμ=CL×ρ×a×s×A
⇒CL=mμ/ρasA
That's it.Am I wrong somewhere?...please reply.
L=CL×1/2ρv^2A
Now,as lift is a force,then it should be as L=mμ, where μ is the "upwards acceleration".
So, L=mμ=CL×1/2ρv^2A
⇒mμ=CL×1/2ρ[(0)^2+2as]A, because v^2=u^2+2as,and here the initial velocity will be zero.
⇒mμ=CL×1/2ρ2asA
⇒mμ=CL×ρ×a×s×A
⇒CL=mμ/ρasA
That's it.Am I wrong somewhere?...please reply.