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Hypersonic shock interactions about a 25 deg/65 deg sharp double cone
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Moss, James N. LeBeau, Gerald J. Glass, Christopher E. |
| Copyright Year | 2002 |
| Description | This paper presents the results of a numerical study of shock interactions resulting from Mach 10 air flow about a sharp double cone. Computations are made with the direct simulation Monte Carlo (DSMC) method by using two different codes: the G2 code of Bird and the DAC (DSMC Analysis Code) code of LeBeau. The flow conditions are the pretest nominal free-stream conditions specified for the ONERA R5Ch low-density wind tunnel. The focus is on the sensitivity of the interactions to grid resolution while providing information concerning the flow structure and surface results for the extent of separation, heating, pressure, and skin friction. |
| File Size | 744236 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020070501 |
| Archival Resource Key | ark:/13960/t53f9q795 |
| Language | English |
| Publisher Date | 2002-08-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Air Flow Hypersonic Shock Direct Numerical Simulation Computational Fluid Dynamics Low Density Wind Tunnels Shock Wave Interaction Computerized Simulation Computational Grids Free Flow Monte Carlo Method Slender Cones Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
