• 제목/요약/키워드: Separation Flow Angle

검색결과 239건 처리시간 0.025초

원주주위를 지나는 흐름에 관한 수치해석 (- Numerical Solutions for the Flow past a Cylinder-)

  • 조용식;윤태훈
    • 물과 미래
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    • 제31권4호
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    • pp.291-297
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    • 1998
  • 2차원 흐름이 원주주위를 지날 때 발생하는 흐름의 변화가 기본방정식인 연속방정식과 운동량방정식에 의하여 수치적으로 해석된다. 수채해석 과정은 기본방정식에 유함수, 와도 및 흐름의 특성을 나타내는 무차원 매개변수를 도입하여 무차원 유함수-와소수송식을 유도한후, successive over relaxation scheme과 alternating direct implicit scheme으로 수행된다. 수치실험은 레이놀즈수 125-275를 갖는 흐름에 대하여 수행되었으며, 시간에 따른 유선, 와도, 원주표면의 압력을 구하는 방법에 있어서 기존의 수치해석에서는 주로 방사 운동량방정식만을 사용하였으나, 본 논문에서는 기존의 방법외에 방사 운동량방정식 및 접선 운동량방정식에 의해 압력을 계한하고, 두값을 비교하여 레이놀즈수에 따른 압력을 구하는 방법을 제시한다. 또한 와도의 분포를 도시하여 원주에 의한 후류의 영향을 받지 않는 외부경계의한계를 새로이 설정한다.

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3차원 미니밴 형상 주위의 비압축성 점성 유동 해석 (Incompressible Viscous Flow Analysis Around a Three Dimensional Minivan-Like Body)

  • 정영래;박원규;박영준;김종섭;홍성훈
    • 한국전산유체공학회지
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    • 제2권1호
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    • pp.46-53
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    • 1997
  • The flow field around a three dimensional minivan-like body has been simulated. This study solves 3-D unsteady incompressible Navier-Stokes equations on a non-orthogonal curvilinear coordinate system using second-order accurate schemes for the time derivatives, and third/second-order scheme for the spatial derivatives. The Marker-and-Cell concept is applied to efficiently solve continuity equation. A H-H type of multi-block grid system is generated around a three dimensional minivan-like body. Turbulent flows have been modeled by the Baldwin-Lomax turbulent model. To validate present procedure, the flows around the Ahmed body with 12.5° of slant angle are simulated. A good agreement with other numerical results is achived. After code validation, the flows around a mimivan-like body are simulated. The simulation shows three dimensional vortex-pair just behind body. The flow separation is also observed on the rear of the body. It has concluded that the results of present study properly agreed with physical flow phenomena.

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CFD 시뮬레이션 기반 초임계 LNG용 사인함수 PCHE 설계 (Design of sinusoidal shape channel PCHEs for supercritical LNG based on CFD simulation)

  • 판진싱;염은섭
    • 한국가시화정보학회지
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    • 제19권3호
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    • pp.69-76
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    • 2021
  • Printed circuit heat exchanger (PCHE) is a compact heat exchanger with good heat transfer performance, high structure integrity, and reliability over a wide range of temperatures and pressures. Instead of the traditional zigzag and straight shape channel, the sinusoidal shape channel was adopted in this study to investigate the relation of thermal-hydraulic performance and waviness factors (period and amplitude). The local flow characteristics and the heat flux distribution were compared to verify the effects of period and amplitude on heat transfer performance. As the period of channel becomes shorter, the rapid change of the flow direction can produce high flow separation around the corner leading to the disturbance of the boundary layer opposite wall. The nonuniform distribution of flow velocity appeared around the corner positions can promote fluid mixing and lead to higher thermal performance. An evaluation index was used to compare the comprehensive performance of PCHE considering the Nusselt number and Fanning factor. Based on the simulation results, the optimal design parameters of PCHE channel shape were found that the channel with an equivalent bending angle of 15° offers the highest heat flux capacity.

충격파 및 유동박리 효과를 고려한 초임계 에어포일의 천음속 플러터 특성 (Transonic Flutter Characteristics of Supercritical Airfoils Considering Shockwave and Flow Separation Effects)

  • 김동현;김유성;김요한;김석수
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 추계학술대회논문집
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    • pp.167-174
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    • 2008
  • In this study, flutter analyses for supercritical airfoil have been conducted in transonic region. Advanced computational analysis system based on computational fluid dynamics (CFD) and computational structural dynamics (CSD) has been developed in order to investigate detailed static and dynamic responses of supercritical airfoil. Reynolds-averaged Navier-Stokes equations with Spalart-Allmaras (S-A) and SST ${\kappa}-{\omega}$ turbulence models are solved for unsteady flow problems. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of cascades for fluid-structure interaction (FSI) problems. Also, flow-induced vibration (FIV) analyses for various supercritical airfoil models have been conducted. Detailed flutter responses for supercritical are presented to show the physical performance and vibration characteristics in various angle of attack.

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PIV에 의한 델타형 날개에서의 유동특성에 관한 연구 (A Study about Flow Characteristics on Delta-wing by PIV)

  • 이현;김범석;손명환;이영호
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 춘계학술대회
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    • pp.2151-2156
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    • 2003
  • The distinguishing features of flows at high angles of attacks are caused by the generation of free shear layers at sharp leading edges, by separation of the viscous layers from the surfaces of wings and bodies and by the flow in the wakes of the wings and bodies. In this study, systematic approach by PIV experimental method within a circulating water channel was adopted to study the fundamental characteristics of induced vortex generation, development and its breakdown appearing on a delta wing model with or without LEX in terms of four angles of attack($15^{\circ}$, $20^{\circ}$, $25^{\circ}$, $30^{\circ}$) and six measuring sections(30%, 40%, 50%, 60%, 70%, 80%) of chord length. Distributions of time-averaged velocity vectors and vorticities over the delta wing model were compared along the chord length direction. Highly swept leading edge extension(LEX) applied to delta wings has greatly improved the subsonic maneuverability of contemporary fighters. High-speed CCD camera which made it possible to acquire serial images is able to get the detailed information about the flow characteristics occurred on the delta wing. Especially quantitative comparison of the maximum vorticity featuring the induced pressure distribution were also conducted to clarity the significance of the LEX existence.

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선박 연돌 형상이 배기가스 흐름에 미치는 영향과 연돌 설계 (CFD interpretation of gas flow around Ship's Funnel and Optimum Design Criterion)

  • 신현준;박상민;김종화
    • 대한조선학회 특별논문집
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    • 대한조선학회 2011년도 특별논문집
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    • pp.63-69
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    • 2011
  • Exhaust gases of a vessel from a main engine, a diesel generator and an incinerator contain very harmful substances like soot, $SO_2$ and NOx. Careful design of funnel shape is required to prevent those harmful exhaust gases from influencing on accommodation and a fan room. Meanwhile, the exhaust gases are also hot enough to damage electronic devices like radar. Therefore the funnel design should be considered so that electronic devices are not directly exposed to the exhaust gas in the strong stern wind. This study may propose guidelines of optimum design criterion for the anti-thermal damage design of the electronic devices and anti-recirculating design of harmful exhaust gas near the accommodation. From CFD analyses, we can understand that the major factors affecting the exhaust gas dispersion are the large scale mixing by separation vortices and the sluggish flow in the recirculation region. We hope that the funnel flow analysis around ship's funnel is used for practical optimum funnel design to minimize the exhaust gas dispersion by adjusting the funnel shape, the position of the exhaust pipe, the shape of bulwark, the exhaust direction of air ventilated an engine room and the angle of the exhaust pipe.

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충격파 및 유동박리 효과를 고려한 초임계 에어포일의 천음속 플러터 특성 (Transonic Flutter Characteristics of Supercritical Airfoils Considering Shockwave and Flow Separation Effects)

  • 임함;김동현;김유성;김요한;김석수
    • 한국항공운항학회지
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    • 제17권2호
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    • pp.8-17
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    • 2009
  • In this study, flutter analyses for supercritical airfoil have been conducted in transonic region. Advanced computational analysis system based on computational fluid dynamics (CFD) and computational structural dynamics (CSD) has been developed in order to investigate detailed static and dynamic responses of supercritical airfoil. Reynolds-averaged Navier-Stokes equations with Spalart-Allmaras (S-A) and SST ${\kappa}-{\omega}$ turbulence models are solved for unsteady flow problems. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of cascades for fluid-structure interaction (FSI) problems. Also, flow-induced vibration (FIV) analyses for various supercritical airfoil models have been conducted. Detailed flutter responses for supercritical are presented to show the physical performance and vibration characteristics in various angle of attack.

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입구베인 각도에 따른 터보블로어 성능특성 연구 (Performance Analysis for Turbo Blower According to Inlet-Vane Angles)

  • 장춘만;임수정;양상호
    • 대한기계학회논문집B
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    • 제35권3호
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    • pp.301-307
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    • 2011
  • 본 연구에서는 생활폐기물 관로이송 설비에서 사용되고 있는 터보블로어 입구베인의 설정각도에 따른 성능특성을 삼차원 나비어-스톡스 방정식을 통한 수치해석과 실험적인 방법을 적용하여 분석하였다. 다양한 압력특성에 따라 운전되는 시스템 특성을 고려하여 2 대의 터보블로어를 직렬로 연결한 실험용 시뮬레이터를 설계, 제작하고 각각의 터보블로어 성능특성을 입구베인의 설정각도에 따라 분석하였다. 입구베인의 설정각도에 따른 터보블로어 성능특성을 수치해석과 실험적 평가밥법으로 분석하여, 입구베인 설정각도가 완전 개방조건인 90 도에서 60 도까지 사용하였을 경우 효율의 손실없이 압력 및 유량을 제어할 수 있음을 확인하였다. 입구베인의 설정각도가 작은 경우에는 입구측의 스월흐름으로 인하여 입구 유속분포가 불균일하게 되며, 이로 인하여 하류측에 설치되는 터보블로어의 효율이 상대적으로 감소됨을 알 수 있었다.

섬유강화 복합재료 사출성형품의 섬유배향상태 (Fiber Orientation distribution of Injection Molded Product on the Fiber-Reinforced Polymeric Composites)

  • 이정주;김진우;김혁;한길영;심재기;이동기
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2004년도 춘계학술대회 논문집
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    • pp.76-81
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    • 2004
  • Injection molding is the most widely used process fir the industrial forming of plastic articles. During an injection molding process of composites, the fiber-matrix separation and fiber orientation are caused by the flow of molten polymer/fiber mixture. As a result. the product tends to be nonhomogeneous and anisotropic. Hence, it is very important to clarify the relations between separation orientation and injection molding conditions. So far, there is no research on the measurement of fiber orientation using image processing. In this study, the effects of fiber content ratio and molding condition on the fiber orientation-angle distributions are studied experientially. Using the image processing method, the fiber orientation distribution of welding pars in injection-molded products is assessed. And the effects of fiber content and injection mold shapes on the fiber orientation in case of fiber reinforced polymeric composites are studied experimentally.

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회전체 분급기의 원리 및 연구 개발 동향 (Research and development of centrifugal classifiers: A review)

  • 송동근;한방우;김학준;김용진;정상현;홍원석
    • 한국입자에어로졸학회지
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    • 제4권2호
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    • pp.37-50
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    • 2008
  • Concerns on centrifugal classifiers, of which have cut sizes are below few micrometers, have been increased and it is prospected to be used in extensive industries, such as manufacturing the fine minerals, cosmetics, advanced electric materials, and life science. This paper reviews the recent progress of research and development on the centrifugal classifiers. General categorization of classifiers for feeds was assessed and separation mechanism of the classifiers was followed. History of centrifugal classifiers was explored and some points to be improved were briefly indicated. Fundamental theory of the classification by centrifugal classifiers was pearly studied, and advanced and further understandings on factors affecting the separation or grading efficiency are described. Factors determining the classification precision and efficiency of centrifugal classifiers, such as geometry, rotational speed and inclined angle of rotating vanes, feed and air flow rates, and rotor dimensions are reviewed.

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