2-D linearised Euler equation
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(Difference between revisions)
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:<math> \frac{\partial p}{\partial t}+\frac{\partial u}{\partial x}+\frac{\partial v}{\partial y}+M\frac{\partial p}{\partial x}=0 </math> | :<math> \frac{\partial p}{\partial t}+\frac{\partial u}{\partial x}+\frac{\partial v}{\partial y}+M\frac{\partial p}{\partial x}=0 </math> | ||
:<math> \frac{\partial \rho}{\partial t}+\frac{\partial u}{\partial x}+\frac{\partial v}{\partial y}+M\frac{\partial \rho}{\partial x}=0 </math> | :<math> \frac{\partial \rho}{\partial t}+\frac{\partial u}{\partial x}+\frac{\partial v}{\partial y}+M\frac{\partial \rho}{\partial x}=0 </math> | ||
+ | where M is the mach number , speed of sound is assumed to be 1, all the variabled refer to acoustic perturbations over the mean flow. | ||
+ | :Domain [-50,50]*[-50,50] | ||
+ | :Initial Condition | ||
+ | :Boundary Condition | ||
+ | :Numerical Method | ||
+ | :Results | ||
+ | :Reference |
Revision as of 02:08, 8 October 2005
Problem Definition
where M is the mach number , speed of sound is assumed to be 1, all the variabled refer to acoustic perturbations over the mean flow.
- Domain [-50,50]*[-50,50]
- Initial Condition
- Boundary Condition
- Numerical Method
- Results
- Reference