Viscous-Inviscid Interaction
- Quasi-Simultaneous Method
Veldman recognized the importance of solving simultaneously the viscous and inviscid
flow equations. The coupling is advanced station-by-station between a linearized form
of the inviscid flow and the boundary layer equations. There are two alternatives,
depending on whether the boundary layer equations are solved directly or inversely.
For example, the direct solution of the boundary layer equations would lead to a
correction formula as
Veldman used a local linearization of the viscous effects on the external inviscid
flow from the thin airfoil theory
where
is the velocity distribution at the outer edge of the boundary layer in absence of viscous effects,
and
denote the limits of influence of the viscous correction on the
inviscid flow, and
is the blowing velocity at the wall.
Eq.15 is formally the interaction law. In fact, it is solved simultaneously
with the boundary layer equations, since both
and
are
unknown. Then the method consists in iterating Eq. 15 with the boundary layer
equations at the current step, until convergence is achieved. Then the process is
advanced.
Figure 1: Geometric interpretation of the quasi-simultaneous method
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