Experimental investigation on atomization of an air-blast atomizer with plain-orifice nozzle and dual-swirl cup
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Experimental investigation on atomization of an air-blast atomizer with plain-orifice nozzle and dual-swirl cup
Vol. 21, Issue 5, (2006)
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:
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Published:2006
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ZHANG Chi, ZHANG Rong-wei, XU Guo-qiang, et al. Experimental investigation on atomization of an air-blast atomizer with plain-orifice nozzle and dual-swirl cup[J]. 2006, 21(5).
DOI:
ZHANG Chi, ZHANG Rong-wei, XU Guo-qiang, et al. Experimental investigation on atomization of an air-blast atomizer with plain-orifice nozzle and dual-swirl cup[J]. 2006, 21(5).DOI:
Experimental investigation on atomization of an air-blast atomizer with plain-orifice nozzle and dual-swirl cup
An air-blast atomizer consisting of a plain orifice nozzle and dual counter-rotating radial swirlers was experimentally investigated to obtain sauter mean diameter(SMD) and Rosin-Rammler distribution parameter at different pressure drops and air-fuel ratios.The mean diameter and distribution parameter of fuel spray were measured by Marlven particle size analyzer.The experimental results show that the SMD and distribution parameter of fuel spray decrease with increasing air pressure drop and air-fuel ratio
and a critical air-fuel ratio occurs in the transitional process
when the actual air-fuel ratio exceeds the critical
the SMD and the distribution parameter change little with changing air pressure drop and air-fuel ratio
A prediction model of film-cooling adiabatic effectiveness based on cohence non-isothermal jet theory
Research on ignition performance of a hybrid airblast atomizer combustor with convergent-divergent sleeve
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
ZHANG Chi
LIN Yu-zhen
XU Quan-hong
LIN Yu-zhen
LIN Pei-hua
XU Quan-hong
LIU Gao-en
YUAN Yi-xiang
Related Institution
National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Jet Propulsion, National Key Laboratory on Aero-Engines, 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