|Table of Contents|

Experimental and model research of penetration characteristic for Y-shape nozzle(PDF)

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

Issue:
2011年03期
Page:
38-41
Research Field:
研究与设计
Publishing date:

Info

Title:
Experimental and model research of penetration characteristic for Y-shape nozzle
Author(s):
CHI Bao-hua HONG Liu YANG Guo-hua ZHONG Wei-cong
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
Y-shape nozzlepenetration performancemathematical model
PACS:
V434-34
DOI:
-
Abstract:
To research the penetration performance of Y-shape nozzle, the experimental system was built, the working parameters of the nozzle were designed and the cold test was conducted under the design conditions. The influence of air-liquid ratio(2%~4%)on the penetration depth was analyzed according to the experiment results. The novel dimensionless complex momentum was presented. M. Y. Leong experiential formula was improved base on the new nondimensional multiple momentum. The experiential parameters was fitted under the experimental condition. All the more, the mathematics model of kenetic droplet was calculated and analyzed.

References:

[1]LEONG M Y, MCDONELL V G. Effect of ambient pressure on airblast spray injected into a crossflow, AIAA 98-3093 [R]. USA: AIAA, 1998.
[2]BERESH Steven J, HENFLING John F. Penetration of a transverse supersonic jet into a subsonic compressible cross flow [J]. AIAA Journal, 2005, 43 (2): 379-389.
[3]刘静, 徐旭. 超声速横向气流中喷雾的数值模拟[J]. 火箭推进, 2006, 32(5): 32-36.
[4]龚景松, 傅维镳. 一种新型喷嘴的提出及其流量特性的研究[J]. 工程热物理学报, 2005, 26(3): 507-510.
[5]XUE J, JOG M A, JENG S M. Effect of geometric parameters on simplex atomizer performance, AIAA 2002-3710 [R]. USA: AIAA, 2002.
[6]王达文, 孙荣权. 高雾化质量喷嘴的设计研究[J]. 沈阳大学学报, 2001, 13(4): 55-57.
[7]石玉文.气动喷嘴雾化特性的数值研究[J]. 汽轮机技术,2007, 49(4): 294-295.
[8]樊未军, 萧琦, 杨阳 等.旋流多级气动喷嘴设计和喷雾特性研究[J]. 工程热物理学报, 2002, 23(3): 391-393.
[9]徐行, 郭志辉, 顾善建. 新型气动雾化喷嘴喷雾特性的实验研究[J]. 航空动力学报. 1997, 12(3): 295-334.
[10]龚景松, 傅维镳. 旋转型气-液雾化喷嘴的雾化特性研究[J]. 热能动力工程, 2006, 21(6): 632-634.

Memo

Memo:
-
Last Update: 1900-01-01