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      KCI등재 SCIE SCOPUS

      Relative Deviation of Mass Flow Rate in Swirl Injectors due to the Engineering Tolerances: Experimental Study

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      https://www.riss.kr/link?id=A105909660

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      다국어 초록 (Multilingual Abstract)

      The accuracy of mass flow rate in injector depends upon the derivation of nozzle diameter (dc) and discharge coefficient (Cd). To compare the relationship between different dimensions of injectors, the relative variation mass flow rate through the inj...

      The accuracy of mass flow rate in injector depends upon the derivation of nozzle diameter (dc) and discharge coefficient (Cd). To compare the relationship between different dimensions of injectors, the relative variation mass flow rate through the injector is calculated according to the accuracy of high-class precision to get maximum relative deviation of mass flow rate. In this paper, the effect of engineering tolerances of three dimensions (nozzle diameter, depth of tangential channel and radius of twisting arm) on the mass flow rate of swirl injector was investigated through an experimental study. Then, the maximum relative deviation of mass flow rate (Δm˙/m˙)max between different swirl injectors was measured. The experimental results show that the (Δm˙/m˙)max was affected by the tolerances of nozzle diameter and depth of inlet channel greater than radius of twisting arm.

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      참고문헌 (Reference)

      1 Moon S, "The spray characteristics of a pressure-swirl injector with various exit plane tilts" 34 (34): 615-627, 2008

      2 Soltani MR, "Spray characteristics of a liquid-liquid coaxial swirl atomizer at different mass flow rates" 9 (9): 592-604, 2005

      3 Zhao J, "Simulation and experimental study on the atomization character of the pressure-swirl nozzle" 2 (2): 271-277, 2012

      4 Park KS, "Nonlinear modeling of drop size distributions produced by pressure-swirl atomizers" 36 (36): 1-12, 2010

      5 Ommi F, "Experimental investigation of characteristics of a double-base swirl injector in a liquid rocket propellant engine" 14 (14): 479-491, 2010

      6 정연재, "Experimental Study on Simplex Swirl Injector Dynamics with Varying Geometry" 한국항공우주학회 12 (12): 57-62, 2011

      7 Maniarasan P, "Design and performance evaluation of swirl injectors for water evaporation at low pressure" 235 (235): 139-145, 2009

      1 Moon S, "The spray characteristics of a pressure-swirl injector with various exit plane tilts" 34 (34): 615-627, 2008

      2 Soltani MR, "Spray characteristics of a liquid-liquid coaxial swirl atomizer at different mass flow rates" 9 (9): 592-604, 2005

      3 Zhao J, "Simulation and experimental study on the atomization character of the pressure-swirl nozzle" 2 (2): 271-277, 2012

      4 Park KS, "Nonlinear modeling of drop size distributions produced by pressure-swirl atomizers" 36 (36): 1-12, 2010

      5 Ommi F, "Experimental investigation of characteristics of a double-base swirl injector in a liquid rocket propellant engine" 14 (14): 479-491, 2010

      6 정연재, "Experimental Study on Simplex Swirl Injector Dynamics with Varying Geometry" 한국항공우주학회 12 (12): 57-62, 2011

      7 Maniarasan P, "Design and performance evaluation of swirl injectors for water evaporation at low pressure" 235 (235): 139-145, 2009

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2023 평가예정 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
      2020-01-01 평가 등재학술지 유지 (해외등재 학술지 평가) KCI등재
      2013-10-01 평가 등재학술지 선정 (기타) KCI등재
      2011-01-01 평가 등재후보학술지 선정 (기타) KCI등재후보
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      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.37 0.2 0.3
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.26 0.24 0.394 0.03
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