| タイトル | Thrust chamber performance using Navier-Stokes solution |
| 本文（外部サイト） | http://hdl.handle.net/2060/19850010709 |
| 著者（英） | Chan, J. S.; Freeman, J. A. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1984-12-12 |
| 言語 | eng |
| 内容記述 | The viscous, axisymmetric flow in the thrust chamber of the space shuttle main engine (SSME) was computed on the CRAY 205 computer using the general interpolants method (GIM) code. Results show that the Navier-Stokes codes can be used for these flows to study trends and viscous effects as well as determine flow patterns; but further research and development is needed before they can be used as production tools for nozzle performance calculations. The GIM formulation, numerical scheme, and computer code are described. The actual SSME nozzle computation showing grid points, flow contours, and flow parameter plots is discussed. The computer system and run times/costs are detailed. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 85N19019
NASA-CR-171346
LMSC-HREC-TR-D951729
NAS 1.26:171346 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/157169 |
