2-D linearised Euler equation
From CFD-Wiki
(Difference between revisions)
m (Reverted edits by DarpaSbotr (Talk) to last version by Harish gopalan) |
|
(One intermediate revision not shown) |
Latest revision as of 12:31, 19 December 2008
Contents |
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
Characteristic Boundary Condition
Numerical Method
4th Order Compact scheme in space 4th order low storage RK in time
Results
Pressure
- No mean flow
- Mean Flow to left at U=0.5 (c assumed to be 1 m/s)
Reference
- Williamson, Williamson (1980), "Low Storage Runge-Kutta Schemes", Journal of Computational Physics, Vol.35, pp.48–56.
- Lele, Lele, S. K. (1992), "Compact Finite Difference Schemes with Spectral-like Resolution,” Journal of Computational Physics", Journal of Computational Physics, Vol. 103, pp 16–42.