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Figure 18A shows a set of streamlines representing potential flow past a stationary inclined plate before any eddy has been shed.
The fluid is modeled by potential flow.
The aerodynamic model is a potential flow model.
The water flow is described by potential flow theory.
This is verified on two potential flow benchmarks.
For potential flow solvers, this boundary layer solution is typically based on empirical viscous corrections.
First a previously developed potential flow design method is extended to the viscous flow computations.
The potential flow solver with a boundary layer model, XFOIL, provides sectional aerodynamic loads.
Potential flow methods are limited by its exclusion of viscous effect.
The aim of solution is mainly against the velocity potential of the potential flow.
Viscous losses were quantified using additional models that use the potential flow as input.
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