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Simulation of the second combustor internal flowfield for a solid-propellant ducted rocket(PDF)

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

Issue:
2007年04期
Page:
23-27
Research Field:
研究与设计
Publishing date:

Info

Title:
Simulation of the second combustor internal flowfield for a solid-propellant ducted rocket
Author(s):
Xu Yingjun; Gao Feng; Wang Peng
Missile Institute of Air Force Engineering University,Xi’an 713800,China
Keywords:
-
PACS:
V435
DOI:
-
Abstract:
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References:

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Memo

Memo:
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Last Update: 1900-01-01