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Afterbody external aerodynamic and performance prediction at high reynolds numbers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carlson, John R. |
| Copyright Year | 1999 |
| Description | This CFD experiment concludes that the potential difference between the flow between a flight Reynolds number test and a sub-scale wind tunnel test are substantial for this particular nozzle boattail geometry. The early study was performed using a linear k-epsilon turbulence model. The present study was performed using the Girimaji formulation of a algebraic Reynolds stress turbulent simulation. |
| File Size | 339611 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20000044630 |
| Archival Resource Key | ark:/13960/t8z945r83 |
| Language | English |
| Publisher Date | 1999-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics High Reynolds Number Reynolds Stress Flight Tests Computational Fluid Dynamics Boattails Afterbodies Wind Tunnel Tests Performance Prediction Computerized Simulation Aerodynamic Characteristics Potential Flow Axisymmetric Bodies Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
