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Direct numerical simulation of acoustic waves interacting with a shock wave in a quasi-1d convergent-divergent nozzle using an unstructured finite volume algorithm
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mankbadi, Reda R. Bui, Trong T. |
| Copyright Year | 1995 |
| Description | Numerical simulation of a very small amplitude acoustic wave interacting with a shock wave in a quasi-1D convergent-divergent nozzle is performed using an unstructured finite volume algorithm with a piece-wise linear, least square reconstruction, Roe flux difference splitting, and second-order MacCormack time marching. First, the spatial accuracy of the algorithm is evaluated for steady flows with and without the normal shock by running the simulation with a sequence of successively finer meshes. Then the accuracy of the Roe flux difference splitting near the sonic transition point is examined for different reconstruction schemes. Finally, the unsteady numerical solutions with the acoustic perturbation are presented and compared with linear theory results. |
| File Size | 469295 |
| Page Count | 7 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19960001694 |
| Archival Resource Key | ark:/13960/t9g49mw0h |
| Language | English |
| Publisher Date | 1995-09-01 |
| Access Restriction | Open |
| Subject Keyword | Acoustics Perturbation Theory Sound Waves Computational Fluid Dynamics Unstructured Grids Mathematics Digital Simulation Steady Flow Shock Wave Interaction Convergent-divergent Nozzles Finite Volume Method Boundary Conditions Unsteady Flow Flux Difference Splitting Shock Waves Algorithms Least Squares Method Transition Points Time Marching Linear Equations Grid Generation Mathematics Aeroacoustics Compressible Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |