Experiment investigation on atomization characteristic of an air-blast atomizer with centrifugal nozzle and co-dual-swirl cup
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Experiment investigation on atomization characteristic of an air-blast atomizer with centrifugal nozzle and co-dual-swirl cup
Vol. 24, Issue 10, (2009)
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,北京,100191
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Published:2009
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GUO Xin-hua, LIN Yu-zhen, ZHANG Chi, et al. Experiment investigation on atomization characteristic of an air-blast atomizer with centrifugal nozzle and co-dual-swirl cup[J]. 2009, 24(10).
DOI:
GUO Xin-hua, LIN Yu-zhen, ZHANG Chi, et al. Experiment investigation on atomization characteristic of an air-blast atomizer with centrifugal nozzle and co-dual-swirl cup[J]. 2009, 24(10).DOI:
Experiment investigation on atomization characteristic of an air-blast atomizer with centrifugal nozzle and co-dual-swirl cup
An air-blast atomizer consisting of a centrifugal nozzle and co-dual-swirl cup was experimentally investigated to obtain atomization characteristics.The radial columnar swirlers were adopted.The experiment was performed in the room temperature and atmospheric pressure to obtain Sauter mean diameter and Rosin-Rammler distribution parameter at different atmosphere pressure drops and fuel pressure.In the experiment
the fuel was RP-3.Sauter mean diameter and distribution parameter of fuel spray were measured by Marlven particle size analyzer in the downstream 50 mm of the nozzle.The experimental results show that Sauter mean diameter decreases and distribution parameter increases with rising atmosphere pressure drops and fuel pressure.Two Sauter mean diameter calculation models were adopted in two different air pressure drops(Δp/p<3% and Δp/p>3%).
Vaporization and spray characteristics of vaporizer
Numerical simulation of diesel spray characteristics based on air⁃assisted atomization injection
Comparative experiment of atomization characteristics of RP⁃3 kerosene and surrogate fuel
Effect of key parameters on knock of two⁃stroke kerosene engine
Effect of lean blowout performance of trapped vortex combustor of the afterburner
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RUAN Chang-long
XU Quan-hong
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ZHANG Chi
LIN Yu-zhen
Haocheng JI
Hao WU
Haiqing YANG
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Aviation Powerplant and Machinery Research Institute, Harbin Dongan Engine(Group) Corporation Limited, Aviation Industry Corporation of China
School of Mechanical and Power Engineering,Nanjing Tech University
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
State Key Laboratory of Engines,Tianjin University