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Investigation of numerical schemes for direct numerical simulations of supersonic turbulent boundary layers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Morris, Christopher I. |
| Copyright Year | 2015 |
| File Size | 6164279 |
| Page Count | 43 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20150002949 |
| Archival Resource Key | ark:/13960/t7dr7vg85 |
| Language | English |
| Publisher Date | 2015-01-09 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Supersonic Flow Direct Numerical Simulation Laminar Flow Reynolds Number Upwind Schemes Mathematics Turbulent Boundary Layer Shock Wave Interaction Fourier Analysis Computational Grids Velocity Distribution Compressible Flow Mach Number Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |