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Low thrust viscous nozzle flow fields prediction (Document No: 19920005903)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Liaw, G. S. Mo, J. D. |
| Copyright Year | 1991 |
| Description | A Navier-Stokes code was developed for low thrust viscous nozzle flow field prediction. An implicit finite volume in an arbitrary curvilinear coordinate system lower-upper (LU) scheme is used to solve the governing Navier-Stokes equations and species transportation equations. Sample calculations of carbon dioxide nozzle flow are presented to verify the validity and efficiency of this code. The computer results are in reasonable agreement with the experimental data. |
| File Size | 758826 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920005903 |
| Archival Resource Key | ark:/13960/t4jm75p74 |
| Language | English |
| Publisher Date | 1991-12-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Navier-stokes Equation Fluid Dynamics Nozzle Flow Flow Distribution Carbon Dioxide Low Thrust Spherical Coordinates Computer Programs Viscous Flow 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 |
