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For the aerodynamic forces, a panel method is applied.
The free surface waves are solved with a panel method.
A low-order panel method is used for aerodynamic analysis in the first-level optimization, and a high-order panel method is employed in the second-level optimization.
Therefore, potential theory (via Panel method) cannot sufficiently provide such data.
A single panel method proposed in this paper is a compromise between the single vortex description and the much more accurate but time-consuming panel method.
This uncovers the weaknesses of the panel method in estimating the effect of growth across countries.
Open image in new window Figure 9 Results of the C L from the panel method.
Panel method based flow solver XFOIL is used as flow solver for optimization.
The monetization approach, distance-to-target method and panel method are considered as optional weighting approaches.
Regarding the latter, the error source in the steady integral panel method is discussed.
Then, the blade profiles are designed by means of panel method with "viscous/inviscid interaction".
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