A mathematical model of the priming process of propellant pipelines was presented based on one-dimensional fluid theory using the method of characteristics (MOC) and finite deference.Coordinate transformation technique was employed to change fluid motion in time-dependent domains to ones in time-independent domains.The details of the method were presented with an illustration of the priming process of a simple piping system (system consisted of a tank
a pipe and a isolation valve).The results exhibited greater consistency with conventional method of characteristic calculations.The influence factors to the surge pressure of priming process have been studied future.The results show that the surge pressure can be effectively reduced by increasing the initial gas pressure
decreasing the tank pressure and increasing the polytrophic exponenting.
Investigation of priming process of propellant lines using Fourier spectral method
Simulation method of short crack propagation in turbine disks based on crystal plasticity
Numerical simulation of internal flow field in gas generator of fire extinguishing bomb
Numerical simulation of light-craft effects onlaser supported donation wave with gas-liquid two phase propellant
Low-Reynolds-number wake flows of a triangular prism
Related Author
CHEN Hong-yu
LIU Hong-jun
CHEN Jian-hua
LIU Shang
Ping ZHANG
Shan LU
Xin JING
Mao YANG
Related Institution
Xi'an Aerospace Propulsion Institute, China Aerospace Science and Technology Corpration
School of Power and Energy,Northwestern Polytechnical University
Nondestructive Testing and Evaluation Laboratory, Dalian University of Technology
College of Civil Engineering, Hefei University of Technology
Key Laboratory of Aerospace Chemical Power Technology, Hubei Institute of Aerospace Chemical Techologh, China Aerospace Science and Technology Corporation,Xiangyang Hubei