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Computations of supersonic viscous flow over a finite-width plate
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Li, C. P. |
| Copyright Year | 1977 |
| Description | Finite difference methods were applied to solve the parabolic Navier-Stokes equations for the flow over a finite width plate at 0 deg and 10 deg angles of attack. The methods were developed on the basis of the operator factorization concept resulting in the split of a three dimensional equation into successive two dimensional equations. Backward and centered implicit factorization schemes, were used and their results were compared. Available numerical solutions and experimental data obtained at low Reynolds number conditions were also used for comparison. The backward implicit method provides a more successful solution, which ranges from the merged layer to the strong interaction regimes. Detailed structures were revealed of the shear layer around and behind the side edge. |
| File Size | 8829001 |
| Page Count | 46 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780005066 |
| Archival Resource Key | ark:/13960/t0vq7r04g |
| Language | English |
| Publisher Date | 1977-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Supersonic Flow Navier-stokes Equation Shear Layers Plates Structural Members Finite Difference Theory 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 |
