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Transonic separated flow predictions based on a mathematically simple, nonequilibrium turbulence closure model
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Johnson, D. A. King, L. S. |
| Copyright Year | 1985 |
| Description | A mathematically simple, turbulence closure model designed to treat transonic airfoil flows even with massive separation is described. Numerical solutions of the Reynolds-averaged, Navier-Stokes equations obtained with this closure model are shown to agree well with experiments over a broad range of test conditions. |
| File Size | 376900 |
| Page Count | 16 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860004207 |
| Archival Resource Key | ark:/13960/t7qp10x2k |
| Language | English |
| Publisher Date | 1985-10-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Navier-stokes Equation Nonequilibrium Flow Transonic Flow Numerical Analysis Computational Fluid Dynamics Turbulence Models Reynolds Number Numerical Flow Visualization Mathematical Models Separated Flow Prediction Analysis Techniques 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 |
