| タイトル | CFD-Based Design of Turbopump Inlet Duct for Reduced Dynamic Loads |
| 本文（外部サイト） | http://hdl.handle.net/2060/20030069001 |
| 著者（英） | Rothermel, Jeffry; Dorney, Daniel J.; Dorney, Suzanne M. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2003-07-07 |
| 言語 | eng |
| 内容記述 | Numerical simulations have been completed for a variety of designs for a 90 deg elbow duct. The objective is to identify a design that minimizes the dynamic load entering a LOX turbopump located at the elbow exit. Designs simulated to date indicate that simpler duct geometries result in lower losses. Benchmark simulations have verified that the compressible flow codes used in this study are applicable to these incompressible flow simulations. |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| 権利 | No Copyright |
