Numerical Analyses of the Conjugate Heat Transfer in a Bipropellant Liquid Rocket Combustor
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 98 === The high-temperature gas of a bipropellant liquid rocket combustor may burn and erode the chamber wall, damaging the whole structure. Therefore, in a general practice, part of the fuel of a bipropellant liquid rocket is injected toward the chamber wall to f...
Main Authors: | Tsu-YangHuang, 黃祖洋 |
---|---|
Other Authors: | Tsung-Leo Jiang |
Format: | Others |
Language: | zh-TW |
Published: |
2010
|
Online Access: | http://ndltd.ncl.edu.tw/handle/29899202791597923319 |
Similar Items
-
Effect of fuel impingement cooling on the combustion flow field in a bipropellant liquid rocket combustor
by: Ting-Hao Lan, et al.
Published: (2003) -
Effects of the Asymmetric Impingement of Unlike-Doublet Injection on the Flow of a Bipropellant Liquid Rocket Combustor
by: Ying-Wei Lee, et al.
Published: (2004) -
Stabilization of a bipropellant liquid rocket motor
by: Cox, Dale W.
Published: (1952) -
Stabilization of a bipropellant liquid rocket motor
by: Cox, Dale W.
Published: (2012) -
Numerical Analysis of Fuel-Spray Cooling for Bipropellant Liquid Rocket Engine Combuster
by: Ji-Yi Lu, et al.
Published: (1995)