• Title/Summary/Keyword: 분사길이

Search Result 171, Processing Time 0.021 seconds

축소 노즐에서의 슬롯 막냉각 열전달 특성에 관한 연구

  • 조용일;조형희
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2000.04a
    • /
    • pp.33-33
    • /
    • 2000
  • 고온의 연소가스로부터 노즐 표면을 보호하기 위하여 슬롯을 통하여 냉각 유체를 분사하는 슬롯 막냉각에 대하여 연구하였다. 냉각효율 및 열전달 특성은 주유동과 2차 유동의 분사율에 따라 크게 달라지며, 형상변화 및 유동가속에 의해서도 냉각 효과의 변화를 가져오게 된다. 따라서 본 연구에서는 실험을 통하여 면적비가 16:1인 축소노즐에서 압축성 효과를 배제할 수 있는 유동속도 범위 내에서 분사율 변화(0.5 $\leq$ M $\leq$ 3.0)에 따른 슬롯 막냉각 열전달 특성을 고찰하고, 평판 슬롯 막냉각 경험식의 결과와 비교하였으며, 수치해석을 통하여 축소노즐과 원형관에서의 냉각효율 및 열전달 특성을 비교함으로서 이를 검증하였다. 축소노즐에서의 슬롯 막냉각 열전달 특성은 단열벽면조건을 형성하여 노즐 표면을 따라 설치된 열전대를 이용하여 측정하였다. 그 결과 상대적으로 낮은 분사율(M=0.5, 1.0)에서 분사율 증가에 따른 냉각효율의 증가가 크게 나타났으며, 분사율이 높아짐(M $\geq$ 2.0)에 따라 냉각효율의 증가폭이 점점 감소하고, 일정 분사율 이상에서는 냉각 효율의 증가가 크게 둔화되었다. 분사율이 낮을 경우 평판 슬롯 막냉각 경험식으로 주어진 결과보다 상류에서는 높으나 하류로 진행하면 비슷한 냉각효율을 보였고, 분사율이 높은 경우 평판보다 전 범위에서 약간 높은 냉각효율을 나타냈다. 수치해석 결과에서는 분사율이 낮을 경우 축소노즐의 냉각효율이 원형관에서의 냉각효율 보다 낮거나 비슷하게 나타났으며, 분사율이 높아짐에 따라 축소노즐에서의 냉각효율이 오히려 높아지는 것으로 나타났다.타내었다. 액체 제트의 속도는 처음에는 일정하게 유지되다가 운동량을 보존하기 위해 가스로부터 운동량을 받아 점차 가속되어지는 것으로 나타났다.본 규격은 키, 총장, 어깨길이, 등길이, 머리길이, 머리둘레, 진동둘레, 목둘레, 가슴둘레, 허리둘레, 배둘레, 엉덩이둘레, 앞품, 뒤품, drop치를 포함하고 있고, 각 규격에서 호칭간 치수 간격도 함께 제시하고 있다. 본 연구 결과에서 보듯, 현행 8규격의 무진복의 각 호칭간 적정 허용범위를 고려해 합리적인 치수체계를 정립한다면 치수에 대한 적합도가 상당히 증가할 뿐 아니라 생산비용도 상당히 감축할 것으로 생각된다.나타났다. 4) 호감적 서비스능력 차원에서 세 독립변수간에 유의한 3원 상호작용이 존재하는 것으로 나타나( $F_{2,228}$=15.62, P<.001) 20대에 적합한 의복 착용시( $F_{2,228}$=3.98, P<.05)와 60대에 적합한 의복 착용시( $F_{2,228}$=16.55, P<.001) 점포유형과 격식차림간에는 유의한 상호작용이 존재하는 것으로 나타났다. 5) 호감을 구성하는 세 요인들이 구매의도에 미치는 영향을 조사한 결과 호감적 인상차원은 29%(P<.001), 호감적 서비스능력차원은 6%(P<.001)의 구매의도를 설명해 주는 것으로 나타났다. 본 연구결과 노년 소비자에게 호감을 주는 판매원의 외모는 구매의도에 영향을 주어 실버의류산업의 이익증대와 밀접한 연관을 갖는 서비스품질의 중요한 요인으로 밝혀졌다.중요한 요인으로 밝혀졌다.로운 단백질 EPSPS가 다른 여러 식물에 이미 존재하고 있는 단백질로서 우리가 이미 이러

  • PDF

Experimental Study of Spray Characteristics on the Throttleable Dual Manifold Injector (이중 매니폴드 가변추력 분사기의 분무 특성에 관한 실험적 연구)

  • Youn, Jung-Soo;Kim, Sung-Hyuk;Yoon, Young-Bin
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.15 no.3
    • /
    • pp.22-30
    • /
    • 2011
  • There is a many way of LPRE throttling methods, high-pressure-drop systems, dual-manifold injector, gas injection, multiple chambers, pulse modulation and movable injector components. Especially dual-manifold injector is essentially combines two fixed-area injectors into a common structure, with independent feed systems controlling flow to each injector manifold. In this paper, using indirect photography and liquid film thickness measurement with various injection pressure and tangential entry diameter to decide stability of spray over a wide thrust range in dual manifold injector.

Theoretical Model of Coaxial Twin-Fluid Spray In a Liquid Rocket Combustor (연소실 내 동축형 2-유체 분무의 이론적 모델)

  • 조용호;윤웅섭
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.6 no.2
    • /
    • pp.37-44
    • /
    • 2002
  • A theoretical study of spray and combustion characteristics due to coaxial twin-fluid injection is conducted to investigate the effects of liquid jet property, droplet size, contact length and liquid jet velocity. Model is properly validated with measurements and shows good agreement. Prediction of jet contact length, droplet size, liquid jet velocity reflects genuine features of coaxial injection in physical and practical aspects. Both the jet contact length and tile droplet size are reduced in a linear manner with an increase of injector diameter. Cross sectional area of liquid intact core is reduced with augmented jet splitting rate, thus the jet is accelerated to maintain the mass continuity and with an assistant of momentum diffusion by burnt gas.

Effects of Mean Flow and Nozzle Damping on Acoustic Tuning of a Resonator in a Rocket Combustor (로켓엔진 연소기에서 공명기의 음향 동조에 미치는 유동 및 노즐 감쇠 효과에 관한 연구)

  • Sohn, Chae-Hoon;Park, I-Sun;Kim, Seong-Ku
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.10 no.3
    • /
    • pp.41-47
    • /
    • 2006
  • Effects of mean flow and nozzle damping on acoustic tuning of a gas-liquid scheme coaxial injector are investigated numerically adopting a linear acoustic analysis. The injector plays a role as a half-wave acoustic resonator for acoustic damping in a combustion chamber of a liquid rocket engine. As Mach number of mean flow in a chamber increases, the resonant frequency of the first tangential mode decreases slightly and the optimum injector tuning length varies negligibly. Nozzle damping affects neither the resonant frequency nor the optimum length. From these numerical results, effects of mean flow and nozzle damping on acoustic tuning of a resonator are negligible. As open area of the injectors increases, the acoustic amplitude decreases, but new injector-coupled modes appear.

Numerical Study for Spray Characteristics of Liquid Jet in Cross Flow with Variation of Injection Angle (분사각 변화에 따른 횡단류에 분사되는 액체제트의 분무특성에 대한 수치적 연구)

  • Lee Kwan-Hyung;Ko Jung-Bin;Koo Ja-Ye
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.30 no.2 s.245
    • /
    • pp.161-169
    • /
    • 2006
  • The spray characteristics of liquid jet in cross flow with variation of injection angle are numerically studied. Numerical analysis was carried out using KIVA code, which was modified to be suitable for simulating liquid jet ejected into cross flow. Wave model and Kelvin-Helmholtz(KH)/Rayleigh-Taylor(RT) hybrid model were used for the purpose of analyzing liquid column, ligament, and the breakup of droplet. Numerical results were compared with experimental data in order to verify the reliability of the physical model. Liquid jet penetration length, volume flux, droplet velocity profile and SMD were obtained. Penetration length increases as flow velocity decreases and injection velocity increases. From the bottom wall, the SMD increases as vertical distance increases. Also the SMD decreases as injection angle increases.

Penetration and Breakup Characteristics of Pulsed Liquid Jets in Subsonic Crossflowse (아음속 수직분사제트에서의 가진 분무의 분무 특성연구)

  • Kim, Jin-Ki;Song, Jin-Kwan;Kim, Min-Ki;Hwang, Yong-Seok;Yoon, Young-Bin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2007.11a
    • /
    • pp.83-88
    • /
    • 2007
  • The spray characteristics and liquid column penetration of steady and pulsed injection measurements have been experimentally studied using high speed camera in liquid jets injected into subsonic crossflow. The objectives of this research are to comparison the spray characteristics of steady injection with pulsed injection. Moreover. the effects of frequency are also studied. As the result, This research has been showed that pulsed injection has different penetration compared with steady injection.

  • PDF

Acoustic-Damping Characteristics of Half-Wave Resonator in a Combustion Chamber of Liquid Rocket Engine (로켓엔진 연소기에서 반파장 공명기의 음향감쇠에 관한 수치적 연구)

  • Sohn Chae-Hoon;Park I-Sun
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.9 no.4
    • /
    • pp.9-15
    • /
    • 2005
  • A linear acoustic analysis is performed to explore the characteristics of acoustic damping by a gas-liquid scheme coaxial injector in a liquid rocket engine. The injector can play a role of acoustic resonator. Acoustic-damping characteristics of half-wave resonator are compared with those of quarter-wave resonator. Various effects of the boundary absorption coefficient, injector length and sound speed in combustion chamber and resonator are investigated. As a result, short tuning length of resonator and low sound speed of the medium have a favorable effect on acoustic damping. As the boundary absorption coefficient decreases, the tuning range of the resonator length becomes narrower.

A Study on Spray Angle of Dual Swirl Injector with Different Recess Length (Dual Swirl Injector Recess 길이에 따른 분산각 평가)

  • Park, Hee-Ho;Kim, Tae-Han;Kim, Yoo
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.7 no.3
    • /
    • pp.30-37
    • /
    • 2003
  • Spray angle of dual swirl injector is established according to the velocity ratio at orifice exit. Due to the internal mixing at recess and lack of correlation for the combined two fluid injection, prediction of spray angle is very difficult. This study deal with experimental work and numerical simulation on spray angle with different recess length. Among the multiphase flow models, the VOF model was selected to simulate the spray angle. Feasibility of numerical analysis are confirmed by comparing the results with the experimental data, and the effect of recess on spray angle are analyzed for single and combined spray case.

Spray Characteristics for Recess Length in a Swirl Coaxial Injector to use GCH4/LOx (가스메탄/액체산소를 추진제로 하는 스월 동축형 인젝터의 리세스 길이에 따른 분무특성)

  • Min, Ji-Hong;Lee, Yang-Suk;Ko, Young-Sung;Kim, Sun-Jin;Kim, Yoo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2011.04a
    • /
    • pp.20-23
    • /
    • 2011
  • The spray and atomization characteristics of swirl coaxial injectors which use gas methane and LOx as propellants are investigated experimentally with a recess length variation. Mass distribution and spray angle are measured by a patternator and droplet size to find atomization characteristics are measured by GSV(Global Size and Velocity) system. As a result, when the liquid sprayed, the spray angle decreased and the atomization characteristic was improved with the recess length increase. When the gas and liquid injected simultaneously, the spray angle was decreased and the atomization characteristic was improved comparing to only the liquid injection.

  • PDF

분무 노줄에서 분사되는 액체막의 분산현상에 관한 실험적 연구

  • 이상용;김인구
    • Transactions of the Korean Society of Mechanical Engineers
    • /
    • v.9 no.3
    • /
    • pp.387-394
    • /
    • 1985
  • 본 연구에서는 액체막의 분산현상에 관한 기존의 연구결과들을 토대로 하여 주위 기체의 응축이 액체막의 분산현상-즉, 분산기구와 액체막의 길이(breakup length )에 미치는 영향을, 여러 형태의 노즐에서 분사되는 액체막의 유속과 온도를 변화시켜 가면서, 알아보고자 한다.