|Table of Contents|

A simulation on dynamic characteristics of ramjet fuel regulator based on AMESim(PDF)

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

Issue:
2010年04期
Page:
12-15
Research Field:
研究与设计
Publishing date:

Info

Title:
A simulation on dynamic characteristics of ramjet fuel regulator based on AMESim
Author(s):
You Yurong;  Zhao Shuanglong;  Wu Baoyuan;  Lu Wanruo
Xi'an Aerospace Propulsion Institute, Xi'an 710100, China
Keywords:
-
PACS:
V233.7
DOI:
-
Abstract:
A dynamic simulation model of ramjet fuel regulator was developed using the AMESim software. The regulator dynamic characteristics were simulated. The methods to improve the dynamic performance were provided by analyzing the regulator stability. The simulation model can be used to analyze regulator characteristics. It can also be used for regulator optimum design.

References:

[1]杨锡武, 何保成, 任凤升, 等. 某型弹用冲压发动机巡航段供油振荡的数值仿真[J]. 推进技术, 2006, 27(2): 158-161. [2]尤裕荣, 徐中节, 逯婉若. 基于Simulink/RTW的冲压发动机控制系统半实物仿真[J]. 火箭推进, 2008, 34(5): 50-53. [3]肖岱宗. AMESim仿真技术及其在液压元件设计和性能分析中的应用[J]. 舰船科学技术, 2007, 29(增刊I)：142-144. [4]任新宇, 郭迎清, 姚华廷. 基于AMESim的航空发动机防喘调节器性能仿真研究[J]. 航空动力学报, 2004, 19(4): 572-576.

Memo

Memo:
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Last Update: 1900-01-01