Loading...
Please wait, while we are loading the content...
Similar Documents
Separated transonic airfoil flow calculations with a nonequilibrium turbulence model
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Johnson, D. A. King, L. S. |
| Copyright Year | 1985 |
| Description | Navier-Stokes transonic airfoil calculations based on a recently developed nonequilibrium, turbulence closure model are presented for a supercritical airfoil section at transonic cruise conditions and for a conventional airfoil section at shock-induced stall conditions. Comparisons with experimental data are presented which show that this nonequilibrium closure model performs significantly better than the popular Baldwin-Lomax and Cebeci-Smith equilibrium algebraic models when there is boundary-layer separation that results from the inviscid-viscous interactions. |
| File Size | 658013 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860005777 |
| Archival Resource Key | ark:/13960/t9867d375 |
| Language | English |
| Publisher Date | 1985-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Boundary Layer Separation Navier-stokes Equation Nonequilibrium Flow Turbulence Transonic Flow Supercritical Airfoils Turbulence Models Closure Law Inviscid Flow Separated Flow Aerodynamic Stalling Viscous Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
