• Title/Summary/Keyword: 차압 해석

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Flow Analyses for the Improvement of Uniform Distribution at LOx Manifold of a $30\;ton_f$ Full-scaled Combustor (30톤급 실물형 연소기 산화제 매니폴드 유동해석을 통한 유량 균일성 개선)

  • Kim, Hong-Jip;Kim, Seong-Ku;Kim, Jong-Kyu;Han, Yeoung-Min;Choi, Hwan-Seok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.12 no.3
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    • pp.16-23
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    • 2008
  • Flow analyses have been performed to investigate the uniformity of propellant flow through the oxidizer manifold of a 30 tonf full-scaled combustor. Injectors were simulated as porous medium layers of equivalent pressure drops. The uniformity of oxidizer propellant has been analyzed for various diameters of holes in vertical/horizontal distributors and configurations of oxidizer inlet to propose an improved design solution. It has been proven that the mass flow uniformity were improved by adjusting the holes in vertical/horizontal distributors.

Comparative Study of Propellant Modeling in Chamber of Interior Ballistic (강내탄도의 약실 내 추진제 모델링 비교연구)

  • Jang, Jin-Sung;Sung, Hyung-Gun;Roh, Tae-Seong;Choi, Dong-Whan
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.668-671
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    • 2010
  • Comparative study on propellant modeling has been investigated using a non-dimensional method and an one-dimensional method. The propellant location in the chamber can not be described by the non-dimensional method. It is, however, possible for the one-dimensional method to describe. Therefore, the analysis of the interior ballistics according to the propellant arrangements has been performed by the one-dimensional method. The negative differential pressure in the chamber could be predicted and the necessity of the one-dimensional modeling for the analysis of the interior ballistics has been confirmed.

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Energy Balance Analysis of 30 t Thrust Level Liquid Rocket Engine (추력 30톤급 액체로켓엔진의 에너지 밸런스 해석)

  • Cho, Won-Kook;Park, Soon-Young;Kim, Chul-Woong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.5
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    • pp.563-569
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    • 2012
  • An energy balance analysis is conducted for a 30 t thrust level liquid rocket engine. The relations between thrust and combustion pressure, between thrust and propellant flow rate, and between combustion pressure and fuel pump pressure rise are compared against those indicated by a published database of the existing rocket engines. A combustion pressure higher than the old design value is obtained, implying that the present design is high-performance oriented. The thrust to propellant flow rate ratio is the same as that of the existing engines, indicating that the specific impulse performance is at the usual level. The fuel pump pressure rise is found to be slightly high when the combustion pressure is considered, and it is attributed to the pressure budget of the present ground test engine not being optimized.

A Study on Application Analysis Using RETRAN Computer Code for the Environmental Qualification Flood Analysis Following the Main Feed Water Line Break (주급수관 파단에 따른 내환경검증 침수분석용 전산코드 RETRAN의 적용 해석연구)

  • Park, Young-Chan;Cho, Cheon-Hwey;Hong, Sung-In
    • Journal of Energy Engineering
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    • v.16 no.3
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    • pp.103-112
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    • 2007
  • Flood issue for nuclear power plants designed and built in 1970 is extremely severe for main steam header compartment and main feedwater line region of intermediate building and lower floor. A calculation for flood level at the main feedwater line isolation compartment is now performing by hand calculation. But, this methodology is quite conservative assumption. The goal of this study was to develop method to analyze flowrate using the RETRAN-3D computer code, and the developed method was applied to flood level analysis following main feedwater line break. As a result of analysis, flood level was low remarkably.

Numerical Study of Flow Characteristics in Elementary Paths of Velocity-Control Trim (속도 제어형 트림의 단위 요소 유로의 유동특성에 관한 수치적 연구)

  • Kim, Dae-Kwon;Sohn, Chae-Hoon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.3
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    • pp.245-253
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    • 2011
  • We investigate the flow characteristics of elementary-flow paths with $90^{\circ}$ bends; a velocity-control trim consists of such paths. For geometric similarity, the width and length of each path are selected, and the number of bends is 0, 4, or 8. The flow tests are conducted with the same flow-path elements. The numerical results are in good agreement with the experimental data. In elements without bends, the volume flow rate decreases with the length of the flow path, with a constant pressure drop between the inlet and the outlet. However, in flow paths with $90^{\circ}$ bends, it increases and then decreases with the length of the flow path. For a fixed number of $90^{\circ}$ bends, better pressure-drop characteristics are observed as the length of the flow path increases. For a fixed flow-path length, a flow-path element with more bends has a smoother pressure drop along the path.

Study on Properties of Interior Ballistics According to Ignition-Gas Injections (점화제 주입에 따른 강내탄도 성능해석)

  • Jang, Jin-Sung;Sung, Hyung-Gun;Lee, Sang-Bok;Roh, Tae-Seong;Choi, Dong-Whan
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.1
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    • pp.22-29
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    • 2011
  • Using the numerical code for the interior ballistics, the performance of the interior ballistics with the characteristic of the ignition-gas injections has been investigated. The ignition gas has been assumed to be injected into the chamber with 3 cases. As the results of analysis, when the ignition-gas has been injected into all chamber area, the pressure distributions of the chamber of the interior ballistics have been uniform and the differential pressure has been stable. The ignition-gas has been injected into the partial area of the chamber, however, the pressure distributions and the differential pressure have been unstable. The case using the longer ignition injector, therefore, seems to be more suitable to improve the stability of the interior ballistics.

Hydraulic Tests of Fuel Pump for 75-ton class Liquid Rocket Engines (75톤급 로켓엔진용 연료펌프의 수력성능시험)

  • Kim, Dae-Jin;Hong, Soon-Sam;Choi, Chang-Ho;Noh, Jun-Gu;Kim, Jin-Han
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.78-81
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    • 2009
  • A series of hydraulic tests of a fuel pump are performed using water at a room temperature. The pump is under development for 75-ton class liquid rocket engines of the open-loop gas generator type. According to the test results, the fuel pump satisfies its design requirement and its head and efficiency at the design flowrate are higher than the expected value by the computational analysis. Also, it is found that the pressure at the rear bearing outlet is higher than expected because the inlet of bypass pipe line is narrow. Furthermore, the flowrate of the secondary flow is estimated using the pressure difference of the elbow of the bypass pipe line.

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A Constitutive Model for Lightly Overconsolidated Clays (미약한 과압밀상태의 점토지반에 대한 구성모델)

  • 이승래;오세붕
    • Geotechnical Engineering
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    • v.8 no.4
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    • pp.17-30
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    • 1992
  • Constitutive relations for lightly overconsolidated state of clayey soils. as well as normally consolidated state of those, play an important role in the analyses of geotechnical structures in clay deposits. For the practical point of view, a constitutive model applicable to lightly overconsolidated soils should be developed to easily evaluate the model parameters, and to precisely predict the various behavior of OC soils. For that purpose, a constitutive model for the lightly overconsolidated soil behavior has been proposed to rep- resent the undrained behavior which can be normalized using equivalent pressure, p. , Yielding within the initial yield surface is modeled exclusively using the given normally consolidated model parameters only. Furthermore, the proposed model can be applied to consider the effects of overconsolidation, secondary consolidation, and stress relaxation. The measured behavior in undrained triaxial tests has been Predicted easily and precisely in comparison with other models.

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Analysis of Elements Influencing on Performance of Interior Ballistics (강내탄도의 성능 영향 요소 분석)

  • Sung, Hyung-Gun;Yoo, Seung-Young;Lee, Sang-Bok;Choi, Dong-Whan;Roh, Tae-Seong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.4
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    • pp.16-24
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    • 2013
  • The analysis of performance and internal flow according to various numerical models for interior ballistics has been conducted. The initial flow has been mainly affected by the drag model of propellants and their drag degradation reduces oscillations of differential pressure between the breech and the shot base. Models of Nusselt number haven't influenced the major performance of interior ballistics. The negative differential pressure isn't generated in the case without the heat transfer of propellants.

A Study on the Flow Analysis of Impeller type Measuring Valve according to Differential Pressure at Inlet and Outlet (임펠러 타입 계량 밸브 입·출구 차압에 따른 유동해석에 관한 연구)

  • Tea-Joon Kim;Chung-Seob Yi;Chi-Woo Lee
    • Journal of the Korean Society of Industry Convergence
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    • v.26 no.3
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    • pp.381-387
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    • 2023
  • This study conducts the flow analysis on the basis of the impeller RPM of water measuring valve and differential pressure at valve inlet and outlet. The software used for the flow analysis is STAR-CCM+. In terms of the structure of the measuring valve, it has an impeller installed inside, and a metering chamber has inlet and outlet holes. The flow analysis on the water measuring valve drew the following conclusions: The flow rate and flow coefficient distribution according to the impeller RPM and differential pressure were on the linear increase. Regarding the flow field in the valve, the increased differential pressure had the highest velocity distribution, and complex flow field was generated in the measuring chamber. In particular, since the path between the inlet and outlet holes in the measuring chamber and the valve body was narrow, there was a section that had flow field interference. Given that, it showed the feature of the valve used for water measuring on the basis of the impeller RPM.