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Computational investigation of heat transfer for film cooling thrust chamber(PDF)

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

Issue:
2009年04期
Page:
34-37
Research Field:
研究与设计
Publishing date:

Info

Title:
Computational investigation of heat transfer for film cooling thrust chamber
Author(s):
Zhang Feng; Zhong Weicong
Xi'an Aerospace Propulsion Institute，Xi'an 710100，China
Keywords:
thrust chamber; film cooling; heat transfer
PACS:
V434
DOI:
-
Abstract:
This paper introduced the mechanism and research status of film cooling．A heat transfer computational model for liquid film cooling thrust chamber was established．The model Was used to perform a calculation of the heat transfer in a liquid film cooling thrust chamber．The calculated results agree well with the experimental data．

References:

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[4]高温合金金相图谱编写组．高温合金金相图谱[M]．北 京：冶金工业出版社．1979．
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Memo

Memo:
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Last Update: 1900-01-01