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Hypersonic, nonequilibrium flow over a cylindrically blunted 6 deg wedge
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gnoffo, Peter A. |
| Copyright Year | 1993 |
| Description | The numerical simulation of hypersonic flow in chemical nonequilibrium over cylindrically blunted 6 degree wedge is described. The simulation was executed on a Cray C-90 with Program LAURA 92-vl. Code setup procedures and sample results, including grid refinement studies and variations of species number are discussed. This simulation relates to a study of wing leading edge heating on transatmospheric vehicles. |
| File Size | 785134 |
| Page Count | 40 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940008099 |
| Archival Resource Key | ark:/13960/t4dn92c67 |
| Language | English |
| Publisher Date | 1993-08-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Convective Heat Transfer Nonequilibrium Flow Computational Fluid Dynamics Reacting Flow Aerodynamic Heating Transatmospheric Vehicles Hypersonic Flow Computational Grids Blunt Leading Edges Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |