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논문 기본 정보

자료유형
학술저널
저자정보
Lei Li (Beijing Jiaotong University) Changchun Li (Beijing Jiaotong University) Hengxuan Zhang (Beijing research institute of precision electromechanical control equipment)
저널정보
한국유체기계학회 International Journal of Fluid Machinery and Systems International Journal of Fluid Machinery and Systems Vol.10 No.2
발행연도
2017.6
수록면
176 - 188 (13page)
DOI
10.5293/IJFMS.2017.10.2.176

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초록· 키워드

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The nozzle-flapper valves are widely applied as a pilot stage in aerospace and military system. A subject of the analysis presented in this work is to find out a reasonable range of null clearance between the nozzle and flapper. This paper has presented a numerical flow coefficient simulation. In every design point, a parameterized model is created for flow coefficient simulation and cavitation under different conditions with varying gap width and inlet pressure. Moreover, a new test device has been designed to measure the flow coefficient and for visualized cavitation. The numerical simulation and test results both indicate that cavitation intensity gets fierce initially and shrinks finally as the gap width varies from small to large. From the curve, the flow coefficient mostly has experienced three stages: linear throttle section, transition section and saturation section. The appropriate deflection of flapper is recommended to make the gap width drop into the linear throttle section. The flapper–nozzle null clearance is optionally recommended near the range of D<SUB>N</SUB>/16. Finally through simulation it is also concluded that the inlet pressure plays a little role in the influence on the flow coefficient.

목차

Abstract
1. Introduction
2. Theoretical background
3. Numerical simulation
4. Experimental design and setup
5. Results and analysis of the simulation and tests
6. Conclusion
References

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