Numerical analysis for transient interior flow field of the cold-flow impact in SRMs

被引：0
|
作者：
He, Fan [1 ]
Yu, Ling [1 ]
Cai, Wen-Xiang [1 ]
Yang, Ling [2 ]
机构：
[1] Department of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing, China
[2] Ningbo University of Technology, Ningbo, China
来源：
Guti Huojian Jishu/Journal of Solid Rocket Technology | 2015年 / 38卷 / 01期
关键词：
Compilation and indexing terms; Copyright 2025 Elsevier Inc;
D O I：
10.7673/j.issn.1006-2793.2015.01.012
中图分类号：
学科分类号：
摘要：
Transient analysis - Rocket engines - Flow fields
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页码：67 / 72
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