|Table of Contents|

Numerical simulation of cryogenic gaseous hydrogen emission(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2013年04期
Page:
74-79
Research Field:
测控与试验
Publishing date:

Info

Title:
Numerical simulation of cryogenic gaseous hydrogen emission
Author(s):
LI Mao SUN Wan-min LIU Rui-min
Beijing Institute of Aerospace Testing Technology, Beijing 100074, China
Keywords:
cryogenic gaseous hydrogen diffuse area combustion model numerical
PACS:
V434-34
DOI:
-
Abstract:
The cryogenic emission and burning emission of cryogenic gaseous hydrogen were investigated numerically for safe emission. The standard k-ε turbulence model and the uni-step H-O reaction model was used in the simulation calculation to get the gaseous hydrogen emission pressure, mass flow rate, temperature, environment wind speed, as well as hydrogen diffuse area and burning area as the evaluation index. The calculated results show that the burning area by burning emission is smaller than the diffuse area by cryogenic emission, and increase of emission pressure, amplification of mass flow rate and reduction of temperature can lead to the wide diffuse area and burning area of gaseous hydrogen.

References:

[1]LAPIN A. Hydrogen vent flare stack performance[J]. Advances in Cryogenic Engineering, 1967 (12): 198-206.
[2]THOMPSON W R, BONCORE C S. Design and deve- lopment of a test facility for the disposal of hydrogen at high flow rates[J]. Advances in Cryogenic Engineering, 1967 (12): 207-217.
[3]张起源. 液氢的危险性综合分析[J]. 国外导弹技术, 1983(7): 50-67.
[4]朱森元. 氢氧火箭发动机及其低温技术[M]. 北京: 国防工业出版社, 1995.
[5]郑治仁. 氢爆炸事故十四例[J]. 中国航天, 1999 (12): 12-14.
[6]秦国军, 袁杰红, 胡茑庆, 等. 氢泄漏稳定扩散场数值模拟与回归建模研究[J]. 高技术通讯, 2010, 20(11): 1206-1210.
[7]肖建军, 周志伟, 经荥清. 严重事故下安全壳内氢气浓度场分布影响因素的初步研究[J]. 核动力工程, 2007,28(1):99-103.
[8]杨灿剑, 付晋. 加氢站氢气泄漏事故模拟及后果分析[J]. 消防科学与技术, 2011, 30(4): 358~361.
[9]卢明, 徐晔, 肖学章. 室内氢气泄漏扩散的数值模拟[J]. 中国安全生产科学技术, 2011,7(8):29~33.
[10]张分电, 王正, 洪祥, 等. 高酸气田井站火炬冷放空过程模拟分析[J]. 安全、健康和环境, 2012,12(6): 11-13.
[11]吴光中, 李久龙, 高婉丽, 等. 大流量氢气的排放与扩散研究[J]. 导弹与航天运载技术, 2010 (1): 51-55.
[12]庄逢辰. 液体火箭发动机喷雾燃烧的理论、模型及应用[M]. 长沙: 国防科技大学出版社, 1995.
[13] 李宁, 宋文艳, 罗飞腾, 等. 基于先锋氢点火和双凹腔火焰稳定的煤油超声速燃烧特性[J]. 推进技术, 2012 (2): 205-210.

Memo

Memo:
-
Last Update: 1900-01-01