• 제목/요약/키워드: Pressure Hole

검색결과 756건 처리시간 0.029초

직선형 5공 압력프로브의 새로운 교정 알고리듬 적용 (Application of the New Calibration Algorithm of a Straight-Type Five-Hole Pressure Probe)

  • 김장권;오석형
    • 대한기계학회논문집B
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    • 제32권11호
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    • pp.863-869
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    • 2008
  • This paper investigated the new calibration algorithm of a straight-type five-hole pressure probe for measuring three-dimensional flow velocity components. This new calibration algorithm was used for velocity data reduction from the calibration map and based on the combination of a look-up, a binary search algorithm and a geometry transformation including the translation and reflection of nodes in a calibration map. The calibration map was expanded up to the application angle, ${\pm}55^{\circ}$ of a probe. This velocity data reduction method showed a perfect performance without any kind of interpolating errors in calculating yaw and pitch angles from the calibration map. Moreover, when it was applied to an actual flow field including a swirling flow, a good result came out on the whole.

터빈 블레이드 형상 곡면에서의 막냉각 효율 특성 (The Characteristics of Film-Cooling Effectiveness on a Turbine-Blade-Shaped Surface)

  • 윤순현;류원택;김동건;김대성;김귀순
    • 대한기계학회논문집B
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    • 제26권3호
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    • pp.384-393
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    • 2002
  • The effects of hole expansion angle and the arrangement of nozzles on a film cooling system for a turbine-blade-shaped surface were experimentally investigated. Liquid crystal with flue-temperature correlation and an image processing system were employed to evaluate surface temperature. Distributions of cooling effectiveness were then presented to figure out the change of heat transfer characteristics with different geometric conditions of cooling-holes. It was found thats the averaged cooling efficiency on the suction surface was maximum with 10 degree of the cooling hole expansion angle. It was also shown that the averaged cooling efficiency on the pressure surface and the averaged cooling efficiency for dual array case were not affected by the hole expansion angle.

다중 홀 핀틀 인젝터와 연속형 핀틀 인젝터의 연소성능 비교 (Comparison of Combustion Efficiency of Multi Hole Pintle Injector and Continuous Pintle Injector)

  • 남정수;이건웅;구자예
    • 한국항공우주학회지
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    • 제50권3호
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    • pp.165-172
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    • 2022
  • 핀틀 인젝터는 추진제 분사면적 조절이 가능하기 때문에 추력제어에 가장 적합한 인젝터이다. 그에 따라 본 논문에서는 액체산소와 기체메탄을 사용하여 다중 홀 핀틀 인젝터와 연속형 핀틀 인젝터의 연소시험을 수행하였다. 특성속도효율로 두 핀틀의 연소성능을 확인하였고, O/F와 연소실 압력에 따라 두 파라미터가 유사한 조건에서 실험결과를 비교하였다. 개도(산화제 분사면적)가 100% 추력조건일 때 다중 홀 핀틀의 효율이 연속형 핀틀보다 다소 높은 결과를 나타내었다.

원형 단면 구멍 표면을 갖는 댐퍼 후로팅 링 실의 누설량 및 회전체 동역학적 특성 해석 (Leakage and Rotordynamic Analysis of Damper Floating Ring Seal with Round­Hole Surfaces in the High Pressure Turbo Pump)

  • 하태웅;이용복;김창호
    • Tribology and Lubricants
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    • 제19권6호
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    • pp.349-356
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    • 2003
  • A damper floating ring seal with round hole pattern surfaces is suggested for better leakage control. The flat plate test of the round hole pattern surfaces has been performed to yield an empirical friction factor model. The exact predictions of the lock­up position of the damper floating ring, the leakage performance, and the rotordynamic coefficients of the seal are necessary to evaluate the rotordynamic performance of the turbo pump unit. The governing equations including the empirical friction factor model for round hole pattern surfaces are solved by the Fast Fourier Transform method. The lock­up position, leakage flow rate, and rotordynamic coefficients are evaluated according to the geometric parameters of the damper floating ring seal. Theoretical results show that the damper floating ring seals yield less leakage and better rotordynamic stability than the floating ring seal with a smooth surface.

하이드로 피어싱된 튜브 부위의 변형해석 (Analysis of Deformation Surrounding the Pierced Hole in the Tube Hydro-Piercing Process)

  • 최성기;김동규;문영훈
    • 소성∙가공
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    • 제13권2호
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    • pp.154-159
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    • 2004
  • Deformation surrounding the hole in the tube during the hydropiercing process has been investigated in this study. The tube is expanded and internally pressurized between upper and lower dies, and a piercing punch is driven forcefully through a cross passage in the die and through the wall of the tube. The pressurized fluid within the tube provides support to the wall of the tube during a piercing step to form a hole in the tube having less deformation surrounding the hole in the tube. The deformation area may be fully retracted to a substantially flat form or partially retracted to a countersunk form. In this study, a mathematical model that can predict deformation surrounding the hole has been proposed and experimentally verified by actual hydropiercing test.

ADJOINT METHOD FOR CONTROLLED CAVITATION INVERSE NOZZLE DESIGN

  • Petropoulou, S.;Gavaises, M.;Theodorakakos, A.
    • International Journal of Automotive Technology
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    • 제7권3호
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    • pp.283-288
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    • 2006
  • A mathematical methodology is proposed for designing nozzle hole shapes producing controlled geometric cavitation. The proposed methodology uses an unstructured RANS flow solver, with the ability to compute sensitivity derivatives via an adjoint algorithm. The adjoint formulation for the N-S equations is presented while variation of the turbulence viscosity is not taken into account during the geometry modifications. The sensitivities are calculated in a mode independently of the shape parameterisation. The method is used to develop and evaluate conceptual shapes for nozzle hole cavitation reduction. The localized region at the hole inlet producing cavitation, is parameterised using its radius of curvature, while a cost function is formulated to eliminate the negative pressures present at this location. Sensitivity derivatives are used to assess the dependence of the localized region on the minimum pressure, and to drive the geometry to the targeted shape. The results show that the computer model can provide nozzle hole entry shapes that produce predefined flow characteristics, and thus can be used as an inverse design tool for nozzle hole cavitation control.

수소용 다이어프램 압축기의 오일 분배 홀 패턴에 따른 수치해석 (Numerical Analysis on a Hydrogen Diaphragm Compressor with Various Oil Distribution Holes Pattern for Hydrogen Compressor)

  • 박현우;신영일;김규보;송주헌;장영준;전충환
    • 한국수소및신에너지학회논문집
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    • 제20권2호
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    • pp.87-94
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    • 2009
  • There are several types of compressors which are appropriate for hydrogen gas station. Diaphragm type of compressor is the one of them and it satisfies the requirements for that purpose in terms of maintaining gas purity and making high pressure over 700 bar. The objective of this study is to find an optimal design of oil distribution hole configuration. The number of holes is changed maintaining total cross-sectional area of holes. Five cases(1 hole, 4, 8,16 and 24 holes) were studied through Fluid Structure Interaction(FSI) analysis method. Gas and oil pressure, the deflection and stress of the diaphragm were analysed during compression and suction process respectively. There is no specific difference among the cases during compression. An additional deflection due to the existence of hole was found during suction for all case. But the highest deflection and stress were found in the 1 hole case. It was seen that 60% decrease of stress in magnitude in 24 hole case compare to the 1 hole case.

환형관내 고-액 2상 유동의 압력손실 변화특성에 대한 연구 (A Study on the pressure loss of sloid-liquid 2 phase flow in an annulus)

  • 우남섭;한상목;황영규;윤치호;김영주
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2720-2724
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    • 2007
  • Field measurements have revealed that the pressure drop over a borehole during drilling of a slim oil well or a well with a long reach can depend significantly on the rotation speed of the drill pipe. An accurate prediction of the annular frictional pressure drop is therefore important for conditions where the annular clearance is small. An experimental study was carried out to study solid-liquid two phase flow in a slim hole annulus. Annular velocities of carrier fluids varied from 0.2 m/s to 1.5 m/s. The carrier fluids which were utilized included tap water and CMC water solutions. Pressure drops and average flow rates were measured for the parameters such as inner-pipe rotary speed, carrier fluid velocity, hole inclination and particle injection rate. For both water and CMC solutions, the higher the concentration of the solid particles is, the larger the pressure gradients become.

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휴반 살포용 노즐의 분무특성에 관한 연구 (A Study on the Characteristics of the Spraying Nozzle on Paddy Levee)

  • 최규홍;손낙율
    • 한국농공학회지
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    • 제17권2호
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    • pp.3758-3762
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    • 1975
  • In order to find out the optimum size of nozzle of the power sprayer in the paddy field, four different sized hole of nozzles were tested on its discharge volume per unit time and its effective covering distance. 1. The discharge rate of each nozzle is proportional to square root of the transmitted internal pressure of liquid, and the discharge coefficient ranges from 0.82 to 0.86 at the pressure of 20 to 30 kg/$\textrm{cm}^2$. 2. The effective covering distance is increased as the size of the hole is larded and also the pressure is increased under under the limited pressure. Generally, the effective covering distance is not greatly increased at the pressure of above 25kg/$\textrm{cm}^2$. The distance from the nozzle to the spot where the largest amount of droplets are dropped is about 14.5m for 3.05mm nozzle and 16m for 4.05mm nozzle in the pressure range from 20 to 25kg/$\textrm{cm}^2$. 3. From the above results it is concluded that the 3mm nozzle with the power sprayers, which are now being supplied to the farmers, can be used for disease and insect control on the paddy field of which block size is 30m${\times}$100m, and operators need not to enter the field for spraying. For the 40m${\times}$100m block, 4mm nozzle should be used with large size of pump which discharge capacity is 60l/min or more.

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에어데크 적용 시 발파공 내 압력변화 특성에 대한 수치해석 (A Numerical Study on Pressure Variation Characteristics in Blasthole by Air-Deck)

  • 강대우;허원호
    • 화약ㆍ발파
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    • 제29권1호
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    • pp.1-9
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    • 2011
  • 에어데크 공법은 노천광 및 대규모 발파현장에서 널리 쓰이는 대표적인 발파기술 중 하나이다. 에어데크 공법의 효율성 극대화를 위해 그간 많은 연구와 실험이 이루어졌으며, 공내에서 어떠한 압력 거동을 일으키는가를 규명하기 위한 노력들이 있었다. 본 연구에서는 다양한 에어데크 조건하에서 각 에어데크 구간이 어떠한 압력의 차이를 일으키는가에 대해 수치해석적으로 분석하였고, 에어데크의 위치와 에어데크 구간의 길이에 대한 압력변화를 알아보았다. 기본적으로 모든 수치해석은 JWL 상태방정식을 사용하였으며 2차원 평면상에서 진행 하였다. 순수한 압력의 변화만을 관찰하기 위해 암반의 밀도와 강도만을 달리하고 모든 암반은 균질한 상태로 가정하였다.