• Title/Summary/Keyword: 노즐 길이

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A Study on Nozzle Performance Influence with Aft-deck Geometry (Aft-deck 형상에 의한 노즐 성능 영향성 연구)

  • Lee, Changwook;Park, Youngseok;Jin, Juneyub;Kim, Jaewon;Choi, Seong Man
    • Journal of the Korean Society of Propulsion Engineers
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    • v.25 no.2
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    • pp.42-54
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    • 2021
  • The Aft-deck is being applied to the latest unmanned aircraft for the purpose of shielding the gas turbine exhaust plume or spreading jets to increase the mixing rate with the ambient air, thereby reducing the temperature of exhaust gases. In this study, we would like to find out how the performance of the nozzle is affected by the design variables of the Aft-deck. The design variables of aft-deck are selected as length, expansion angle and upper deck shape. The correlation between thrust and plume shielding rate with the length variable is presented. And the correlation between the thrust and the jet diffusion range is presented according to the expansion angle. In addition, the thrust increase effect is confirmed by the removal of the upper deck and the characteristics of transverse velocity vector determined mixing performance with external flow.

Design Factor Analysis of Aerospike Pintle Nozzle for Increasing Thrust in Off-Design (탈설계 조건에서 추력 증대를 위한 에어로 스파이크 핀틀 노즐의 설계인자 분석 연구)

  • Kim, Jeongjin
    • Journal of Aerospace System Engineering
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    • v.16 no.4
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    • pp.1-9
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    • 2022
  • A design factor analysis was conducted to reduce the thrust reduction in the off-design, due to the driving of the aerospike pintle nozzle. The close (NPR 100) as well as the open (NPR 11) stroke were fixed, as under-expansion conditions. The pintle contour, pintle head radius (R), cowl angle (θ), and cowl exit length (L) were selected as design factors. The change in thrust was analyzed, using a verified numerical analysis technique. First, the pintle head radius and the length of the cowl exit had little influence on the thrust. The cowl angle changed the mass flow rate by affecting the effective nozzle throat area, and created a reverse pressure gradient at the cowl exit. As a result of applying the dual aerospike contour, it was confirmed that the thrust in the design-off increased by approximately 1.2%, compared to the reference case and by approximately 3.4% compared to the worst case.

High Speed Wind Tunnel Test on the Aerodynamic Load Characteristics of Rocket Nozzle (로켓 노즐 공력하중 특성에 대한 고속 풍동시험)

  • Ra, Seung-Ho;Ok, Ho-Nam;Kim, In-Sun;Choi, Seong-Wook
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.9
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    • pp.35-40
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    • 2004
  • The high-speed wind tunnel test of rocket model was performed to investigate the effect of skirt configuration on aerodynamic load characteristics of nozzle. Test parameters were the length and diffusing angle of skirt. Test results showed that the gimbals actuator power could be reduced to 1/10 of that without skirt. The normalized test result was proposed to be used as database for skirt design.

Effect of Diesel Nozzle Internal Geometry on the Spray Characteristics (디젤노즐의 내부구조가 분무특성에 미치는 효과)

  • 배종욱;안수길
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.13 no.6
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    • pp.1238-1249
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    • 1989
  • 본 연구에서는 분무체적에 영향을 미치는 분사차압, 주위공기밀도, 노즐공의 직경과 분무각을 변수로 하여 상관관계식을 이론적으로 유도하고 이를 근거로 하여 분 무의 평균공연비 증대를 향상시키는 방안을 제시하였다.

Study on Temperature Control and Optimal Design for Continuous Sterilizer (연속 살균기의 온도제어 및 최적설계에 관한 연구)

  • Park, Cheol Jae
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.39 no.8
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    • pp.813-821
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    • 2015
  • In this paper, we analyzed the problems of a batch-type sterilizer and design a continuous sterilizer to control the temperature deviation. The temperature deviation is analyzed with respect to design parameters such as a nozzle diameter, hole diameter, and nozzle length. The significant temperature parameters are optimized using the response surface methodology. An experimental apparatus is developed using the optimized design parameters. Using a field test, we show that the target temperature is obtained in about 7.3 minutes and the temperature deviation is improved about $0.84^{\circ}C$. The optimized parameters from the test are equal to the analytical parameters.

축소 노즐에서의 슬롯 막냉각 열전달 특성에 관한 연구

  • 조용일;조형희
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2000.04a
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    • pp.33-33
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    • 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

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Flow characteristics of supersonic twin-fluid atomizers (초음속 2유체 분무노즐의 유동 특성)

  • Park, Byeong-Gyu;Lee, Jun-Sik
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.20 no.7
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    • pp.2267-2276
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    • 1996
  • Twin-fluid atomization has been widely used in combustors and process industries because of its high performance and simple structure. Flow visualization and pressure measurements were conducted to investigate the effects of gas flow in twin-fluid atomization. Schlieren photographs showed that changes in atomizing gas pressure, altered the wave patterns, and the lengths of both recitrculating toroid (impinging stangnation point) nad supersonic flow region in the jet. A longer supersonic wave pattern like net-shape wqas observed as atomizing gas pressure increased. The disintegration phenomenon of liquid delivery tube. The variation of spray angles with gas pressures were obtained by visualization using laser sheet beam. Suction pressuresat the nozzle orifice exit and recirculating region are shown to be used to estimate the stable atomization condition of a twin-fluid atomizer.

Equation for handle assessment of cotton and polyester fabrics using nozzle extraction testing method (노즐시험법을 이용한 면/폴리에스터 직물의 촉감 방정식)

  • Yoon, Chang-Hyun;Chun, Dae-Yeop;Hong, Cheol-Jae
    • Science of Emotion and Sensibility
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    • v.14 no.2
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    • pp.191-196
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    • 2011
  • Fabric extraction force measured through nozzle tester reflects a comprehensive fabric handle. Nozzle tester takes advantage of low cost, and simple and fast operating procedure compared with KES system. The paper is to develop the semi-emprical equation for assessment of the fabric handle measured with nozzle tester on the basis of friction law. The variables considered in the equation arc fabric's frictional coefficient and drape coefficient which is determined in terms of fabric bending length and shear strain. The experiment of 12 different cotton and polyester fabrics and comparisons between experimental and theoretical results were conducted. Fabrics of high frictional coefficients, high bending length, and low shear strain showed high fabric handle forces (low handle values). The handle forces predicted from the equation agreed well with those measured, which indicates that the equation can be used to objectively evaluate fabric handle with respect to fabric's own properties and also provide an information for fabric design to improve the handle performance.

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Evaluation of Nozzle's Combustion Instability Suppression Effect by Linearized Euler Equation (선형 오일러 방정식을 이용한 노즐의 연소불안정 감쇠 효과 평가)

  • Kim, Junseong;Moon, Heejang
    • Journal of the Korean Society of Propulsion Engineers
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    • v.23 no.6
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    • pp.1-10
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    • 2019
  • The wave motion inside the nozzle is known as one of the major damping elements of the rocket's combustion instability by it's aeroacoustic effects that result from the flow passage through the nozzle throat. These effects can be quantitatively evaluated by the nozzle admittance. In this study, one-dimensional linearized Euler equation was adopted to calculate the nozzle admittance, and trend analysis was performed depending on the nozzle's main design variables. As a result, when nozzle converging part shortens, it is verified that the frequency dependency of the nozzle admittance is decreased due to the widened frequency range with lowered longitudinal nozzle admittance. Also, admittance estimation using the short nozzle theory is not appropriate when the first tangential mode of the pressure perturbation arises.

분무 노줄에서 분사되는 액체막의 분산현상에 관한 실험적 연구

  • 이상용;김인구
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.9 no.3
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    • pp.387-394
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    • 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.