Supersonic flow over a membrane. |
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Figure 2:
Supersonic flow over a membrane.
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- Domain
:
- Unknown horizontal perturbation velocity
- Hyperbolic
- Two homogeneous initial conditions
- One mixed boundary condition at
and a regularity
constraint at
- Constant
, where
is the Mach angle.
Try a Laplace transform. The physics and the fact that Laplace
transforms like only initial conditions suggest that
is the one to
be transformed. Variable
is our ``time-like'' coordinate.