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Numerical solutions for laminar and turbulent viscous flow over single and multi-element airfoils using body-fitted coordinate systems
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Thompson, J. F. Warsi, Z. U. A. Amlicke, B. B. |
| Copyright Year | 1976 |
| Description | The technique of body-fitted coordinate systems is applied in numerical solutions of the complete time-dependent compressible and incompressible Navier-Stokes equations for laminar flow and to the time-dependent mean turbulent equations closed by modified Kolmogorov hypotheses for turbulent flow. Coordinate lines are automatically concentrated near to the bodies at higher Reynolds number so that accurate resolution of the large gradients near the solid boundaries is achieved. Two-dimensional bodies of arbitrary shapes are treated, the body contour(s) being simply input to the program. The complication of the body shape is thus removed from the problem. |
| File Size | 506183 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770003413 |
| Archival Resource Key | ark:/13960/t9k40kb9s |
| Language | English |
| Publisher Date | 1976-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Navier-stokes Equation Two Dimensional Bodies Laminar Flow Reynolds Number Coordinates Turbulent Boundary Layer Airfoils Viscous Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
