Hi,
is there an appropriate method to get the maximum lift coefficient (cl_max) of a wing from the polars of the section airfoils?
The background is that I cut a arbitrary wing into a certain number of sections. After that I use Xfoil to compute the local cl_max. Since this approach neglects...
Dear forum members,
I'm wondering about the physical meaning of the imaginary part of a complex wave number (e.g., the context of fluid dynamics or acoustics). It is obvious that
w = \hat{w} \mathrm{e}^{i k_z z}
describes an undamped wave if k_z = \Re(k_z) and an evanescent wave if k_z =...