Study on reduction of waste grain rate for semi-spherical conic-column grain

相升海; 杨艳羽; 李世鹏; 闫利伟; 刘瑞东; 于兵

doi:10.13224/j.cnki.jasp.2019.06.022

Chinese

您当前的位置：

首页 >

文章列表页 >

Study on reduction of waste grain rate for semi-spherical conic-column grain

更新时间：2026-07-07

- Study on reduction of waste grain rate for semi-spherical conic-column grain
- Vol. 34, Issue 6, Pages: 1389-1398(2019)
- 作者机构：
  
  1. 沈阳理工大学装备工程学院,沈阳,110159
  2. 中国兵器工业集团有限公司辽宁北方华丰特种化工有限公司,辽宁,抚顺,113003
  3. 北京理工大学宇航学院,北京,100081
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.2019.06.022
  CLC：
- Published：2019
- 稿件说明：
移动端阅览
相升海, 杨艳羽, 李世鹏, 闫利伟, 刘瑞东, 于兵. 减小半球锥柱型药柱残药率的研究[J]. 航空动力学报, 2019, 34(6): 1389-1398.

doi: 10.13224/j.cnki.jasp.2019.06.022
相升海, 杨艳羽, 李世鹏, 闫利伟, 刘瑞东, 于兵. 减小半球锥柱型药柱残药率的研究[J]. 航空动力学报, 2019, 34(6): 1389-1398. DOI： 10.13224/j.cnki.jasp.2019.06.022.

doi: 10.13224/j.cnki.jasp.2019.06.022 DOI：

摘要

为了减小半球锥柱型药柱的残药量

分别采用UG NX和MATLAB软件进行了建模和编程计算

得到了药柱燃烧规律和残药率与设计参数的函数关系图

进行了算例分析。计算结果表明

环向槽圆弧半径的取值越大

残药率越小

且残药率减少幅度增加；残药率与内孔半径呈现负相关关系；残药率与环向槽圆弧圆心旋转半径呈现近似抛物线关系

旋转半径值变大时

残药率先增大后减小；残药率与圆柱段长度呈现近似线性关系。计算结果与实际数据的最大相对误差为0.084%。

Abstract

In order to reduce the waste grain of the semi-spherical conic-column grain

a model was built with the UG NX software and the calculations were programmed with the MATLAB software

the relations between the waste grain rate and the design parameters were obtained. The calculated results showed that the larger radius of circular groove meant the smaller waste grain rate and the decrease of waste grain rate. There was a negative correlation between the waste grain rate and the radius of the inner hole

the larger value meant the smaller waste grain rate. There was an approximate parabola relation between the waste grain rate and the radius of the circular center of the circular groove. When the value became big

the waste grain rate increased first and then decreased. The waste grain rate is approximately linear with the length of the cylinder

the larger value meant the higher residual rate. The maximum relative error between the calculated result and the actual data was 0.084%.

关键词

Keywords

references

Views

621

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Simulation study on the influence of spin on ignition process of two⁃phase in solid rocket motor

Gas⁃solid two⁃phase flow characteristics of SRM propellant with front and rear wings

Impact of ignition charge on ignition process of dual⁃pulse solid rocket motor

Influence of transverse variable acceleration on design of insulation structure for solid rocket motor

Numerical analysis for underwater ignition two-phase flow field of solid rocket motor

Related Author

Shengfu QIN

Junwei LI

Zhihui ZHANG

Ye HE

Ningfei WANG

Jun ZHANG

Lei QIN

Tianyu GAO

Related Institution

School of Aerospace Engineering，Beijing Institute of Technology

College of Engineering Science and Technology，Shanghai Ocean University

The 41st Institute of the Sixth Academy of China Aerospace;Science and Industry Corporation Limited

School of Aerospace Engineering，Beijing University of Technology

Xi'an Modern Chemistry Research Institute，China North Industries Group Corporation Limited

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰