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Finite-difference solution for turbulent swirling compressible flow in axisymmetric ducts with struts
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Anderson, O. L. |
| Copyright Year | 1974 |
| Description | A finite-difference procedure for computing the turbulent, swirling, compressible flow in axisymmetric ducts is described. Arbitrary distributions of heat and mass transfer at the boundaries can be treated, and the effects of struts, inlet guide vanes, and flow straightening vanes can be calculated. The calculation procedure is programmed in FORTRAN 4 and has operated successfully on the UNIVAC 1108, IBM 360, and CDC 6600 computers. The analysis which forms the basis of the procedure, a detailed description of the computer program, and the input/output formats are presented. The results of sample calculations performed with the computer program are compared with experimental data. |
| File Size | 3950606 |
| Page Count | 154 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740010534 |
| Archival Resource Key | ark:/13960/t7tn20f1s |
| Language | English |
| Publisher Date | 1974-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Ducted Flow Turbulent Flow Numerical Analysis Finite Difference Theory Struts Compressible Flow Computer Programs Guide Vanes Axisymmetric 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 |
