| タイトル | Finite-difference solution for turbulent swirling compressible flow in axisymmetric ducts with struts |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740010534 |
| 著者（英） | Anderson, O. L. |
| 著者所属（英） | United Aircraft Corp. |
| 発行日 | 1974-02-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 74N18647
NASA-CR-2365
L911211-1 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/195554 |
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