| タイトル | Network Flow Simulation of Fluid Transients in Rocket Propulsion Systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120003148 |
| 著者（英） | Bandyopadhyay, Alak; Ramachandran, Narayanan; Majumdar, Alok; Hamill, Brian |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2011-12-05 |
| 言語 | eng |
| 内容記述 | Fluid transients, also known as water hammer, can have a significant impact on the design and operation of both spacecraft and launch vehicle propulsion systems. These transients often occur at system activation and shutdown. The pressure rise due to sudden opening and closing of valves of propulsion feed lines can cause serious damage during activation and shutdown of propulsion systems. During activation (valve opening) and shutdown (valve closing), pressure surges must be predicted accurately to ensure structural integrity of the propulsion system fluid network. In the current work, a network flow simulation software (Generalized Fluid System Simulation Program) based on Finite Volume Method has been used to predict the pressure surges in the feed line due to both valve closing and valve opening using two separate geometrical configurations. The valve opening pressure surge results are compared with experimental data available in the literature and the numerical results compared very well within reasonable accuracy (< 5%) for a wide range of inlet-to-initial pressure ratios. A Fast Fourier Transform is preformed on the pressure oscillations to predict the various modal frequencies of the pressure wave. The shutdown problem, i.e. valve closing problem, the simulation results are compared with the results of Method of Characteristics. Most rocket engines experience a longitudinal acceleration, known as "pogo" during the later stage of engine burn. In the shutdown example problem, an accumulator has been used in the feed system to demonstrate the "pogo" mitigation effects in the feed system of propellant. The simulation results using GFSSP compared very well with the results of Method of Characteristics. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | M11-0685
M11-1246 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
|
