Numerical investigations of thermal stratification in cooling channel of liquid rocket engine thrust chamber
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Numerical investigations of thermal stratification in cooling channel of liquid rocket engine thrust chamber
Vol. 24, Issue 8, (2009)
作者机构:
1. 北京航空航天大学 宇航学院,北京,100191
2. 北京航天动力研究所,北京,100076
作者简介:
基金信息:
DOI:
CLC:
Published:2009
稿件说明:
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KANG Yu-dong, SUN Bing, GAO Xiang-yu. Numerical investigations of thermal stratification in cooling channel of liquid rocket engine thrust chamber[J]. 2009, 24(8).
DOI:
KANG Yu-dong, SUN Bing, GAO Xiang-yu. Numerical investigations of thermal stratification in cooling channel of liquid rocket engine thrust chamber[J]. 2009, 24(8).DOI:
Numerical investigations of thermal stratification in cooling channel of liquid rocket engine thrust chamber
To study the formation mechanism of thermal stratification in cooling channel and its effects on the flow and heat transfer
three dimensional turbulent fluid flow and heat transfer in a regenerative-cooling channel of liquid rocket engine were numerically investigated with Reynolds stress model(RSM) model
and the coolant was hydrogen
whose thermophysical properties varied with both temperature and pressure.The results show that thermal stratification occurs at non-flow direction
the extent of thermal stratification becomes increasingly significant as the extent of heating increases
and the thermal stratification of coolant is weakened for the existence of secondary flow in throat region;the thermal stratification has little effect on the bulk temperature increase and hydrodynamic losses of hydrogen
but has significant effect on the calculation of the wall heat fluxes and temperature.
A multi cycle propulsion system for amphibious unmanned aerial vehicle with repeatable water exit
Cavitation modeling and start⁃up under⁃rated pressure simulation of liquid rocket engine
Elastoplastic analysis of regenerative cooling structure of liquid rocket engine
Predicting method of safety life of reusable liquid rocket engine turbopump
Flow channel scheme of U⁃shaped cooling channel in scramjet
Related Author
Jun TIAN
Yufan XIE
Fei LONG
Qin LIU
Yidan CHEN
Hongyu CHEN
Yazhou LIU
Shaotong XU
Related Institution
China Special Vehicle Research Institute,Aviation Industry Corporation of China,Limited
Airport Support Bureau,Air Force Logistics Department
Nanjing Puguo Technology Company,Limeted
National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation