• Title/Summary/Keyword: Flowmaster

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Analysis on the Filling Mode of Liquid Oxygen to the Launch Vehicle Using Flowmaster (Flowmaster를 이용한 발사체 액체산소 충전 모드 해석)

  • Park, Soon-Young;Kim, Ji-Hoon;Park, Pyung-Gu;Yu, Byung-Il
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.335-338
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    • 2009
  • The process of charging an oxidizer in the liquid propellant rocket can divide into the cooling of the oxidizer tank, the high flow charge, the small flow charge, and the replenishment charge for the correction of temperature. The oxidizer of the Naro(KSLV-I) first stage uses the liquid oxygen. And the flow rate and the temperature specification corresponding to each charge mode are presented for the requirement. The flow throttling valve and heat exchanger are installed in the oxidizer filling system in order to satisfy this kind of the flow rate and temperature requirement specification. In this research, by using the Flowmaster which is a commercial one-dimension thermo-fluidic analysis program, one dimensional flow system analyses was performed to predict the exact flow rate at each specific mode. Also, the flow rate correction sensitivity of the flow control valves was analytically determined to satisfy the flow condition refinement at each mode within the limited certification test.

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Design and Performance Analysis of Fuel Feed and Fuel Transfer System for Smart UAV (스마트무인기 연료이송/공급 계통의 설계 및 성능분석)

  • Lee Chang-Ho;Lee Soo-Cheol;Choi Hee-Joo;Kim Jai-Moo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.351-354
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    • 2006
  • In the present work, performance analysis of fuel feed and transfer system for Smart UAV was conducted. For the fuel feed system, it was verified that minimum and maximum pressure requirements at the fuel inlet of engine were satisfied. For the fuel transfer system, design variables of jet pump were derived and performance was verified for the maximum acceleration flight condition by using ESDU design guide and flowmaster code.

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Analysis of the Effect of the Parameter on the Air Braking Response Time of Heavy duty Truck (상용 트럭의 공압 브레이크 제동 특성에 미치는 인자에 대한 연구)

  • Kim, Jin-Taek;Cho, Byoung-Soo;Baek, Byoung-Joon
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.15 no.1
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    • pp.8-13
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    • 2014
  • The effect of several parameters to minimize the braking response time has been investigated in this study. The experimental rigs were developed and the results of the experement compared with those of simulation obtained from the net work fluid flow system analysis code (FLOWMASTER). The braking response time and pressure loss were observed at separated braking port and found out that the response time can be reduced by considering the pipe length and environmental thermal conditions. The correlation equation was also presented to predict the pressure loss at various tank pressure.

Fluid Network Analysis for the Fuel-Supply Systems of Gaseous-Injection-Type LPG Engines (가스분사 방식 LPG 엔진의 연료공급시스템 관로 유동해석)

  • Yun, Jeong-Eui
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.10
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    • pp.1019-1024
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    • 2011
  • The gaseous fuel injection(GFI) type of LPG fuel-supply system is more advantageous than liquefied fuel injection(LFI) from the viewpoint of durability and cost reduction. However, compared with LFI types of LPG fuel-supply systems, in the GFI systems it is difficult to achieve precision fuel metering because of the compressible characteristic of the gaseous fuel. In this study, a Helmholtz resonator is proposed as an appropriate system for precision fuel metering in GFI systems, and the effects of the Helmholtz resonator on the fuel metering are simulated by the commercial flow-network-analysis package Flowmaster.

Analysis for Pressure Oscillation on the Inlet of Turbo-Pump at the Moment of Launch Vehicle Engine Startup (발사체 엔진 시동시 PSD 유무에 따른 터보펌프 입구 배관 압력 섭동 해석)

  • Jung, Youngsuk;Kim, Juwan;Park, Kwangkun;Baek, Seungwhan;Cho, Kiejoo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.1144-1147
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    • 2017
  • It was reviewed about the pressure oscillation on the inlet of turbo-pump at the moment of engine startup and shutdown. Specially, This research was performed how much is the effect of PSD(Pogo Suppression Device) about the pressure oscillation on the inlet of turbo-pump at the moment of engine startup and shutdown. For analysis, propellant tank PSD and Engine are modelled with Flowmaster which is the commercial 1D program. As the analysis results, even though the PSD is installed in the pipeline, the pressure drop or rising at the moment of engine startup and shutdown is same compared to the case without PSD. However, it was confirmed that PSD reduces the pressure oscillation of the high frequency band as the original purpose of PSD.

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Design of the Heat Exchanger in Pool Water Management System of a Research Reactor and Estimation of the Pool Water Temperature Using CFD (전산유체해석을 이용한 연구용원자로 수조수관리계통 열교환기 설계 및 수조수 온도 예측)

  • Jeong, Namgyun
    • Journal of Energy Engineering
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    • v.25 no.2
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    • pp.45-51
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    • 2016
  • The pool water management system, which is installed for purification of the coolant in the pools and the primary cooling system of a research reactor, removes the decay heat from the reactor core when the primary cooling system stops. It also removes the heat generated from the irradiated objects in the service pool and the spent fuels in the spent fuel storage pool to keep the temperature of the pools within a limited value. In this study, the heat exchanger of the pool water management system is designed by CFD method using a commercial code Flowmaster, and the temperature of the pools is estimated along the time to conclude the design and operation method of the pool water management system.

A Study on the Engine Lubrication System Analysis Adapting Discontinuous Oil Supply Crankshaft System (불연속 오일공급 크랭크샤프트 시스템을 채택한 엔진 윤활시스템의 해석)

  • 윤정의
    • Tribology and Lubricants
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    • v.20 no.1
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    • pp.27-32
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    • 2004
  • This paper presents unsteady oil flow behaviors in the engine lubrication network to clarify the differences between continuous and discontinuous oil supply crankshaft system. Using commercial network analysis program, Flowmaster2, engine lubrication network system analysis were carried out. And effects of crankshaft speed and supplied oil pressure on pressure fluctuation in oil groove and oil flow rate to each bearing were analyzed.

A Study on the Steam Hammering Characteristics by Sudden Closure of Main Stop Valve in the Main Steam Piping System of a Power Plant (화력발전소 주증기배관에서 밸브 차단에 따른 수증기 충격 특성에 관한 연구)

  • Ha, Ji-Soo;Lee, Boo-Youn
    • Journal of the Korean Institute of Gas
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    • v.17 no.2
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    • pp.70-77
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    • 2013
  • The present study has been carried out to analyze the effect of steam hammering on the steam piping system including the final superheater, the high pressure turbine, check valve and the first reheater by sudden stoping of main stop valve in a power plant. For the present steam hammering analysis, the well known Flowmaster software has been used to model the steam piping system and the time dependent characteristics of pressure and steam mass flow rate has been conducted. Using the result of the unsteady pressure and steam mass flow rate, the forces acting on the elbows in the piping system has been derived. From the present analysis, it has been elucidated that the elbow just before the main stop valve and the elbow near the connection pipe between bypass pipe and check valve had the largest force among the elbows in the steam piping system. The structural safety diagnostics study on the elbow and the supporting structures of the steam piping system of a power plant will be conducted in the future by the present results of the forces acting on the elbow.

Numerical Analysis on the Startup of a Rocket Engine (로켓 엔진의 시동에 관한 해석적 연구)

  • Park, Soon-Young;Seol, Woo-Seok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.11 no.5
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    • pp.60-71
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    • 2007
  • The startup characteristic of liquid propellant rocket engine should be focused on the stable ignition of combustion chamber and gas generator. Also, to lessen the propellants consumption during this period which doesn't contribute to the flight thrust, the engine has to be transferred to the nominal mode quickly. Because of the risk of test, it is impossible to develop all the startup cyclogram or the specifications of engine by test, so the precedent numerical approach is quite necessary. In this study we developed a mathematical model for the startup phenomena in a liquid rocket engine driven by gas generator-turbopump system based on the commercial 1-D flow system analysis program, Flowmaster. Using this program we proposed a methodology to obtain the specifications of turbine starter and the opening time of shutoff valves for the stable startup of the engine. To verify this methodology we qualitatively compared the analysis results to the typical startup curve of the published engine, then found it is quite well matched.

A Study on the Fluid Network Analysis for the LPG Supply System of the Gaseous Fuel Injection Type (LPG 가스분사 방식 연료공급시스템의 관로 유동해석에 관한 연구)

  • Yun, Jeong-Eui;Kim, Myung-Hwan;Nam, Hyeon-Sik;Jeong, Tae-Hyuung
    • Transactions of the Korean Society of Automotive Engineers
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    • v.15 no.2
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    • pp.35-40
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    • 2007
  • The gaseous fuel injection (GFI) type in LPG fuel supply system has more advantage than the liquified fuel injection type from the viewpoint of durability and cost reduction. But in GFI system, to control pressure and temperature of gaseous fuel is needed to get precision fuel metering for the compressible characteristic of gaseous fuel. In this study, the effects of pressure and temperature on the fuel metering was simulated by commercial flow network analysis package, Flowmaster. And the fuel composition effects on the fuel metering were also studied to figure out the fuel metering characteristics.