A prediction model of film-cooling adiabatic effectiveness based on cohence non-isothermal jet theory
|更新时间:2026-07-07
|
A prediction model of film-cooling adiabatic effectiveness based on cohence non-isothermal jet theory
Vol. 22, Issue 12, (2007)
作者机构:
北京航空航天大学 能源与动力工程学院 航空发动机气动热力重点实验室,北京,100083
作者简介:
基金信息:
DOI:
CLC:
Published:2007
稿件说明:
移动端阅览
ZHANG Chi, LIN Yu-zhen, XU Quan-hong. A prediction model of film-cooling adiabatic effectiveness based on cohence non-isothermal jet theory[J]. 2007, 22(12).
DOI:
ZHANG Chi, LIN Yu-zhen, XU Quan-hong. A prediction model of film-cooling adiabatic effectiveness based on cohence non-isothermal jet theory[J]. 2007, 22(12).DOI:
A prediction model of film-cooling adiabatic effectiveness based on cohence non-isothermal jet theory
To predict the slot film-cooing adiabatic effectiveness
a mathematic model was developed based on cohence non-isothermal jet theory.The core temperature distribution of mixing layer in2Dwall jet was deduced through reasonable assumptions
and the temperature was regarded as the adiabatic wall temperature.In addition
this influence of slot geometry parameter and film blowing ratio on the cooling effectiveness was also considered
so the adiabatic effectiveness equation was obtained.The empirical coefficients in this prediction model should be fitted to the experimental data
showing that the present prediction model has an accuracy of within ±8% to all previous experimental data.The feasibility and potential application of this model have been demonstrated
and more experimental data are required for future verification and improvement.
Research on ignition performance of a hybrid airblast atomizer combustor with convergent-divergent sleeve
Experimental investigation on atomization of an air-blast atomizer with plain-orifice nozzle and dual-swirl cup
Combustor Dome Design with Three Swirlers for Widening the Operation Stability Range
Research of Combustion Efficiency of Combustors Using Hybrid Airblast Atomizer under Low Pressure
The Effect of Fuel-Circumferential-Staging on Lean Blowout Limit at Idle Condition
Related Author
LIN Yu-zhen
LIN Pei-hua
XU Quan-hong
LIU Gao-en
ZHANG Chi
ZHANG Rong-wei
XU Guo-qiang
LIN Yu-zhen
Related Institution
School of Jet Propulsion, National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics
National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Beijing University of Aeronautics and Astronautics
Shanghai JiaoTong University
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics