• 제목/요약/키워드: Momentum Ratio

검색결과 309건 처리시간 0.018초

접선형 산화제 주입기의 운동량비에 따른 End-Burning 하이브리드 연소기의 연소유동장 해석 (Reactive Fields Analysis of End-Burning Hybrid Combustor Using Tangential Oxidizer Injectors with Various Momentum Ratio)

  • 민문기;김수종;김진곤;문희장
    • 한국추진공학회지
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    • 제11권2호
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    • pp.37-46
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    • 2007
  • 본 연구에서는 접선형 산화제 주입기를 갖는 end-burning 하이브리드 연소기에서 산화제 운동량비에 따른 연소 유동장을 해석하였다. 산화제의 운동량비가 감소할수록 연소효율은 연소기 전 영역에 걸쳐 증대되는 경향이 포착되었으며 이론 혼합분율과 온도장을 통해 연소실 전 영역에서 최적의 연소가 저 운동량비에서 발생됨을 확인하였다. 강한 선회류가 연소실 내부 유동장을 지배하지만 압력장은 비교적 균일한 분포를 보였다. 접선형 산화제 주입기를 가진 연소기는 운동량비에 관계없이 공통적으로 연료와 산화제가 만나는 연소실 상부에서 환형의 고온부가 발생했으며 향후 주요 개선 사항으로 판단되었다.

An Experimental Study on Turbulent Characteristics of an Impinging Split-Triplet Injector

  • Kang, Shin-Jae;Ryu, Ki-Wahn;Kwon, Ki-Chul;Song, Bhum-Keun
    • Journal of Mechanical Science and Technology
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    • 제15권1호
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    • pp.117-124
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    • 2001
  • This paper presents turbulent characteristics of an impinging F-O-O-F type injector in which fuel ad oxidizer impinge on each other to atomize under the different momentum ratio. Water was used as an inert simulant liquid instead of fuel and oxidizer. The droplet size and velocity in the impinging spray flow field were measured using a PDPA. The gradient of the spray half-width(b$_2$) along the long-axis direction declined throughout the entire spray flow field with increasing the momentum ratio from 1.19 to 6.48. However, the gradient of the half-width(b$_1$) along the short-axis direction decreased with increasing the momentum ratio. The turbulence intensity and turbulent kinetic energy were converged into the center of the center of the initial region with increasing the momentum ratio. As the momentum ratio increased from MR=1.19 to MR=6.48, the turbulent shear stress decreased. The results of this study can be used for the design of an impinging type injector for liquid rackets.

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무화염 연소 형성에 미치는 공급조건에 관한 연구 (Study of injection condition on formation of Flameless combustion)

  • 홍성원;이필형;송기종;황상순
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2013년도 제46회 KOSCO SYMPOSIUM 초록집
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    • pp.47-49
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    • 2013
  • Entrainment length and recirculation ratio that are important factors of flameless combustion systems were analyzed by injection conditions using three dimensional numerical simulation. As a result, the entrainment length increased with an increase of momentum ratio and distance of between nozzle. Also, in case of increasing in momentum of oxidation, recirculation ratio was increased and the average temperature was decreased.

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동축분류 확산화염에서 화염안정화와 연소특성에 관한 연구 (An Experimental Study on Flame Stability and Combustion Characteristics of Coaxial Diffusion Flame)

  • 유현석;오신규
    • 대한기계학회논문집
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    • 제19권2호
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    • pp.509-518
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    • 1995
  • A study for the flame stability and the combustion characteristics of coaxial diffusion flame was conducted. The fuel employed was natural gas. The experimental variables were rim thickness of fuel tube, blockage ratio of the outer diameter of fuel tube to the inner diameter of air tube, and momentum ratio of fuel to air. It was consequently found that the stability in the neighborhood of the fuel rim depended on the rim thickness, especially in the case of above 3 mm, and that the stable region of the flame extended remarkably due to the formation of recirculation zone above rim. The effect of the blockage ratio on the flame stability was found to be minor in the case of above 3 mm of rim thickness. Between the momentum ratio 2 and 3, the stable flame zone was widely established as well good combustion. With increasing the fuel-air momentum ratio, axial velocity, turbulence intensity, and Reynolds stress increased.

연소시험 조건 기반 총운동량비에 따른 가변추력 핀틀 분사기의 분무각 분석 (Study on Spray Angle of a Throttleable Pintle Injector according to Total Momentum Ratio based on Hot Fire Test Conditions)

  • 허수범;김대환;이수지;윤영빈
    • 한국분무공학회지
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    • 제25권3호
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    • pp.126-131
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    • 2020
  • Throttleable rocket engines are in high demand due to the diversification of space missions. Pintle injector is known to be suitable for throttleable rocket engines, because of its high efficiency in overall thrust zone. In this study, the relationship between spray angle of a throttleable pintle injector and total momentum ratio based on hot fire test conditions was investigated. As a result, the spray angle in 100% and 60% throttling level is higher than the spray angle obtained by the case which considers only propellant mass flow rate, owing to higher total momentum ratio (TMR). The results of this study may be useful for predicting spray angle in hot fire test.

카운터블로 해머 프레스 단조공정의 기계진동 특성 해석 (Mechanical Vibration Characteristics Analysis of a Counterblow Hammer Press in the Forging Process)

  • 김수태;주경진;박근종;최영휴
    • 한국기계가공학회지
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    • 제21권8호
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    • pp.43-52
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    • 2022
  • The vibration characteristics of a hammer press are important parameters for machine design and production control. In this study, a counterblow hammer press was mathematically modelled as a mass-spring-damper system in order to analyze its vibration characteristics. The forging efficiency was theoretically derived as a function of the mass ratio, momentum ratio, and the coefficient of restitution And the effects of the mass ratio, momentum ratio and the restitution coefficient on the forging efficiency were also investigated for two particular cases of the unit mass ratio and unit momentum ratio. Additionally, the vibration responses of the counterblow hammer press due to the ram colliding impact were analyzed, and the force transmitted to the foundation through the mounting unit was determined.

분무 조건에 따른 기체 중심 스월 동축형 분사기의 분무 특성 (Spray Characteristics of Gas-Centered Swirl Coaxial Injectors according to Injection Conditions)

  • 박구정;이정호;이인규;윤영빈
    • 한국분무공학회지
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    • 제19권4호
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    • pp.167-173
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    • 2014
  • The spray characteristics of Gas-Centered Swirl Coaxial Injector was investigated that there were different characteristics with or without gas flow. As gas flow was accelerated, the momentum of gas was transferred to the momentum of liquid in the low liquid Reynolds number. Therefore, the axial velocity of liquid was increased and the measured value was smaller than without gas flow. However, in the high momentum flux ratio, the momentum transfer hardly occurred and the results had constant values. As the recess length was increased, the mixing area of gas and liquid also was increased, the results were decreased.

기체 중심 스월 동축형 분사기가 장착된 모형연소기의 운동량비 변화에 따른 연소불안정성 분석 (Effect of Momentum Flux Ratio on Combustion Instabilities in a Model Combustor with a Gas-Centered Swirl Coaxial Injector)

  • 손채훈;김명섭;;윤영빈
    • 한국추진공학회지
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    • 제24권4호
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    • pp.25-32
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    • 2020
  • 모형 연소기에서 동축형 분사기에 의한 연소불안정성을 운동량비 변화에 따라 수치적으로 분석하였다. 실제 로켓 엔진의 경계조건을 기반으로 총 5개의 운동량비를 선택하였다. 운동량비가 증가할수록 분사기 출구에서의 확산각도는 감소하는 경향을 보였으며, 축방향 운동량이 증가할수록 연소기 내부의 압력진폭이 크게 감소함을 확인하였다. 동적 모드 분해 기법(dynamic mode decomposition)을 통해 연소기내의 음향 모드를 파악하였고 관심 섭동 주파수를 갖는 2L 모드(mode)의 감쇠계수를 구하고 이를 통해 운동량비가 증가할수록 연소기의 안정성이 증가함을 보였다.

초임계 환경으로 분사되는 극저온 제트의 분열 (Disintegration of Cryogenic Jet in Super-critical Environment)

  • 이건웅;김도헌;구자예
    • 한국분무공학회지
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    • 제18권3호
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    • pp.140-145
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    • 2013
  • Sub/supercritical spray experiments were conducted, and cryogenic nitrogen and gaseous argon were selected for simulants. liquid nitrogen and gaseous argon were injected in subcritical case, and supercritical nitrogen and near-critical gaseous argon were injected in near-critical/supercritical cases. shadowgraph method was used to visualize spray, and analyzed about the breakup length. The breakup length was measured from numbers of Instantaneous shadowgraph Images from each case, and they were compared with momentum flux ratios and density ratios. It was observed that the relation between breakup length and momentum flux ratio was fitted into former experiment results. and the reasonable constant was suggested about the relation between breakup length and density ratio.

초음속 유동장내 2차분사 분사각도 변화에 따른 열전달 특성 변화 (Heat Transfer on Secondary Injection Surface in Supersonic Flow-field with Various Injection Angle)

  • 송지운;이종주;조형희;배주찬
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년도 제31회 추계학술대회논문집
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    • pp.321-325
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    • 2008
  • 초음속 유동장내에 분사된 2차제트 주변에서의 열전달 현상을 고찰 하였다. 초음속 유동장내에 분사되는 2차유동의 Jet to freestream momentum ratio(운동량비)의 변화와, 2차유동 분사각도에 따른 2차 분사홀 주변의 열전달 특성을 파악하기 위하여 홀 주변의 표면온도 변화를 고속 적외선 카메라를 통하여 측정하였으며, 이를 이용하여 비정상 열유속 기법을 바탕으로 열유속을 계산하였다. 운동량비가 증가할 수록 열전달 현상이 강화 되었으며, $15^{\circ}$ 기울어진 분사보다는 수직 분사의 경우에 더 강한 열전달 현상이 발생되었다. 이를 통해 분사비와 분사 각도가 표면 열전달 분포에 중요한 요인으로 작용함을 확인할 수 있었다.

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