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Analysis of supersonic combustion flow fields with embedded subsonic regions
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Delguidice, P. Dash, S. |
| Copyright Year | 1972 |
| Description | The viscous characteristic analysis for supersonic chemically reacting flows was extended to include provisions for analyzing embedded subsonic regions. The numerical method developed to analyze this mixed subsonic-supersonic flow fields is described. The boundary conditions are discussed related to the supersonic-subsonic and subsonic-supersonic transition, as well as a heuristic description of several other numerical schemes for analyzing this problem. An analysis of shock waves generated either by pressure mismatch between the injected fluid and surrounding flow or by chemical heat release is also described. |
| File Size | 2974243 |
| Page Count | 106 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740019317 |
| Archival Resource Key | ark:/13960/t6741j93g |
| Language | English |
| Publisher Date | 1972-11-01 |
| Access Restriction | Open |
| Subject Keyword | Thermodynamics And Combustion Supersonic Flow Viscosity Shock Waves Supersonic Combustion Subsonic Flow Flow Distribution Heat Transfer 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 |
