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The separated turbulent boundary layer over a wavy wall
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Werle, M. J. Polak, A. |
| Copyright Year | 1977 |
| Description | A study and application of the fourth order spline collocation procedure, numerical solution of boundary layer like differential equations, is presented. A simple inversion algorithm for the simultaneous solution of the resulting difference equations is given. Particular attention is focused on the boundary condition representation for the spline second derivative approximations. Solutions using the spline procedure, as well as the three point finite difference method, are presented for several model problems in order to assess and improve the spline numerical scheme. Application of the resulting algorithm to the incompressible laminar self similar boundary layer equations is presented. |
| File Size | 4288797 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780004073 |
| Archival Resource Key | ark:/13960/t8rc1v86t |
| Language | English |
| Publisher Date | 1977-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Boundary Layer Separation Incompressible Flow Algorithms Laminar Flow Finite Difference Theory Differential Equations Wall Flow Turbulent Boundary Layer Spline Functions Boundary Conditions Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
