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Separating and turbulent boundary layer calculations using polynomial interpretation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rubin, S. G. Rivera, S. |
| Copyright Year | 1977 |
| Description | Higher order numerical methods derived from polynomial spline interpolation or Hermitian differencing are applied to a separating laminar boundary layer, i.e., the Howarth problem, and the turbulent flat plate boundary layer flow. Preliminary results are presented. It is found that accuracy equal to that of conventional second order accurate finite difference methods is achieved with many fewer mesh points and with reduced computer storage and time requirements. |
| File Size | 3134999 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770012412 |
| Archival Resource Key | ark:/13960/t2z36mb08 |
| Language | English |
| Publisher Date | 1977-02-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Boundary Layer Separation Numerical Analysis Flat Plates Finite Difference Theory Turbulent Boundary Layer Spline Functions Polynomials Computer Storage Devices Boundary Layer Flow 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 |
