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The stability analysis technique based on nonlinear theory for liquid propellant rocket engine(PDF)

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

Issue:
2007年01期
Page:
12-17
Research Field:
Publishing date:

Info

Title:
The stability analysis technique based on nonlinear theory for liquid propellant rocket engine
Author(s):
Yang Jingjing;  Liu Weidong
College of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China
Keywords:
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PACS:
V434
DOI:
-
Abstract:
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References:

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Memo

Memo:
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Last Update: 1900-01-01