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Near-field noise computation for a supersonic circular jet
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Loh, Ching Y. Hultgren, Lennart S. |
| Copyright Year | 2005 |
| Description | A fully expanded, high-Reynolds-number, supersonic circular jet of Mach number 1.4 is simulated, using a 3-D finite-volume Navier-Stokes solver, with emphasis on the near field noise. The numerical results are generally in good agreement with existing experimental findings. |
| File Size | 964077 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20050238999 |
| Archival Resource Key | ark:/13960/t11p3297n |
| Language | English |
| Publisher Date | 2005-10-01 |
| Access Restriction | Open |
| Subject Keyword | Acoustics Navier-stokes Equation Large Eddy Simulation Three Dimensional Flow Computation Aircraft Noise Unstructured Grids Mathematics Strouhal Number Supersonic Jet Flow Near Fields Computerized Simulation Unsteady Flow Space-time Ce/se Method Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |