• International Journal of Aeronautical and Space Sciences
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• 제1권2호
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• pp.9-16
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• 2000

For aerodynamic design of missile bodies of non-circular cross-section, the combination of the slender body theory and the cross-flow analogy can hardly be applied owing to the lack of experimental data. An alternative is to utilize the Euler solution in the design stage. For enhanced accuracy, however, an adequate viscous correction is necessary to the Euler solution. In this work, such a procedure is examined to compensate the viscous effect by utilizing the concept of proportionality factor in cross-flow analogy. Predictions of aerodynamic coefficients combining the Euler solution and the viscous correction via proportionality factor are made for a missile body of elliptic cross-section. Results indicate that the present approach can be adopted in designing missile bodies of non-circular cross-sections.

• 설비공학논문집
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• 제16권4호
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• pp.368-373
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• 2004

A flow field in a passage with periodically converging-diverging cross-section is investigated experimentally by PIV measurement. A tube with a sinusoidally wavy cross section is one of several devices employed for enhancing the heat and mass transfer efficiency due to turbulence promotion and unsteady vortical motion. While the numerical flow visualization results have been limited to the fully developed cases, existing experimental results of this flow were simple qualitative ones by smoke or dye streak test. Therefore, the main purpose of this study is to produce quantitative flow data for fully developed and transient flow regime by the Correlation Based Correction PIV (CBC PIV) and to conjecture the analogy between flow characteristics and heat transfer enhancement with low pumping power. Another purpose of this paper is to examine the onset position of the transition and the global mixing, which results in transfer enhancement. At Re=2000, evidences of the global mixing are captured at 2.5 wavy module through the variation of RMS values and instantaneous velocity plot.

• The Journal of the Acoustical Society of Korea
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• 제20권4E호
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• pp.17-23
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• 2001

To develop the code of predicting flow-field and aeroacoustic noise by an electrical cable, a combined CFD-Acoustic analogy approach is selected. The two dimensional, unsteady and incompressible Reynolds-averaged Navier-Stokes solver with κ-ω and κ-ω SST turbulence modeling is used to calculate the near flow-field around an electric cable. Near-field results are then coupled with two-dimensional Curle's integral formulation based upon Lighthill's acoustic analogy with the assumption of acoustic compactness. To validate this code, numerical results are compared with experimental data for a circular cylinder. The simulation shows an overprediction on acoustic amplitudes, but overally speaking, the spectrum pattern of sound pressure agrees well with experiment within an acceptable amount of error. In addition, a few cross-sections of the cable were selected and tested with each other in terms of drag and radiated noise

• Composites Research
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• 제35권5호
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• pp.334-339
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• 2022

본 연구에서는 복합재료 제조 공정 과정 중 수지의 유동 저항성을 대변하는 인자인 투수 계수를 예측하는 알고리즘을 개발하였다. 단방향 연속 섬유 복합재료 내부에서 섬유와 수직인 방향 투수 계수의 정확한 예측을 위해 대표 체적 요소의 단면 형상을 고려하였다. 섬유의 유체 유동 저항성을 정량화하기 위한 인지로 섬유 간 간격이 사용되었고, 등가 길이는 섬유 배열에 따른 수지의 유로 변화를 나타내는 인자로 사용되었다. 전기-유압 유사성을 접목하여 투수 계수 예측 알고리즘을 개발하고 그 타당성을 확인하였다. 알고리즘은 Matlab과 Python으로 구성되고, 타당성 검증을 위해 FLUENT를 통해 예측된 투수 계수와 비교하였다. 알고리즘과 수치 해석을 통해 얻은 투수 계수가 거의 일치함을 확인하여 알고리즘을 검증하였으며, 소요 시간은 수치 해석 대비 약 1/450로 감소하였다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.1716-1720
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• 2000

To develop the code of predicting flow-field and aeroacoustic noise by a electrical cable, a combined CFD-acoustic analogy approach is selected. The two-dimensional, unsteady, incompressible Reynolds-Averaged Navier-Stokes solver with a ${\kappa}{\omega}$, ${\kappa}{\omega}$ SST turbulence modeling is used to calculate the near-field around electrical cable. Near-field results are then coupled with two-dimensional Curle's integral formulation based upon Lighthill's acoustic analogy with an assumption of acoustic compactness. To validate this code, numerical results are compared with experimental data for a circular cylinder. The simulation shows an overprediction on acoustic amplitudes, but overally speaking, the spectrum pattern of sound pressure agrees well with experiment in an acceptable amount of error. In addition, various cross sections of a cable were selected and compared with each other in terms of drag and radiated noise.

• 한국수자원학회논문집
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• 제30권1호
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• pp.63-73
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• 1997

본 연구는 지하심부에 유류를 저장할 때 널리 이용되는 수막시설의 설치에 따른 공동주변의 흐름해석을 모의하기 위한 유한요소모형의 확립에 관한 것이다. 최종 행렬방정식의 대칭형 전체전도행렬을 풀기위해 벡터저장방식의 Choleski법을 이용하였으며, 전기상사법의 결과와 비교하여 모형을 검증하였다. 모형을 실제 비축기지에 적용하였으며, 대표적인 횡단면에 대해 요소망을 구성하여 공동내부의 압력과 수평수막설치에 따른 포텐션과 유속의 변화 등을 비교하고, 종단면에 대한 분석을 통해 연직수막설치에 따른 포텐셜의 변화와 인접공동간의 영향을 비교 분석한 결과 본 연구에서 확립된 모형은 공동주변 흐름해석에 유용하게 이용될 수 있는 것으로 확인되었다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2006년도 제37회 하계학술대회 논문집 B
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• pp.657-658
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• 2006

Recently, the micro on-off valves have been focused on core technology in the fields of the production line of semi-conductor chips and the micro fluid chips for bio-medical applications. A key characteristics for micro valve, operated by compressed air, are high speed response and great repeatability. Indeed, it is also important to keep the pressure on the cross-sectional area of the poppet to be constant regardless of the fluctuation of the pressure exerted on the ports. In this study, we have designed and analysed the high-speed and high flow rate micro on-off valve using the analogy of equivalent magnetic circuit and Finite Element Method(FEM) respectively. In case of poppet, flow field characteristic was analyzed by the variation of poppet and it was able to display flow field by changing the location of the poppet. Also, we verified possibility of the design through the static and dynamic pressure and the 3D distribution curve of the force by working the front poppet.

• 대한기계학회논문집B
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• 제28권4호
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• pp.441-448
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• 2004

A numerical study was conducted to show the effect of aspect ratio on the analogy of the developing laminar flows between in orthogonally rotating straight duct and in a stationary curved duct of rectangular cross-section. In order. to clarify the similarity of two nows, dimensionless parameters (equation omitted) and Rossby Ro= $w_{m}$$\Omega$ $d_{h}$, in a rotating straight duct were used as a set corresponding to Dean number, (equation omitted), and curvature ratio, λ=R/ $d_{h}$, in a stationary curved duct. Four. different aspect ratios A=0.25, 0.5, 2 and 4 were considered. Under the condition that the magnitudes of Ro and λ were large enough to satisfy the 'asymptotic invariance property' and the aspect ratio was larger than 1, there were strong quantitative similarities between the two flows such as flow patterns, friction factors, and maximum axial velocity magnitudes fur the same values of $K_{LR}$ and $K_{LC}$ . On the other hand, as the aspect ratio decreased below 1 (A=0.25 and 0.5), the difference of the secondary flow intensity between these two flows was enhanced and therefore the analogy of two flows was not so evident as that of the larger aspect ratio (A=2 and 4). 4).nd 4).

• 대한기계학회논문집
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• 제17권6호
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• pp.1621-1632
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• 1993

본 연구에서는 모델 냉각통로 내에 대한 유동장 및 열전달 계수분포를 구하기 위하여 수치적 방법에 의한 접근을 시도하였고 이를 위하여 본 연구실에서 개발한 유한체적법 유동해석 프로그램인 TURBO-3D를 사용하였다. 계산 영역은 터빈날개 내의 냉각유로를 단순화한 ㄹ자 형태의 유로를 설정하였으며 등온상태의 유동에 대하여 해를 구하였다.실제 고온의 터빈날개내에서는 큰 온도구배에 의한 강한 부력효과가 예상되어 이를 무시할 수는 없으나 등온 가정하의 유동장으로부터 Reynolds analogy 에 의한 열전달특성의 유추가 가능하다. 그러므로, 본 연구에서는 특히 회전수의 변화에 따른 Coriolis효과의 변화 및 2차 유동의 구조를 파악하였고 또한 이들에 의한 주 유동장과 압력분포 및 국부 열전달 특성을 파악하였다.

• 대한기계학회논문집B
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• 제25권5호
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• pp.731-740
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• 2001

A numerical study on the quantitative analogy between the fully developed turbulent flow in a straight square duct rotating about an axis perpendicular to that of the duct and that in a stationary curved duct of square cross-section is carried out. In order to clarify the similarity of the two flows, dimensionless parameters K(sub)TR=Re(sup)1/4/√Ro and Rossby number, Ro, in a rotating straight duct flow were used as a set corresponding to K(sub)TC=Re(sup)1/4/√λ and curvature ratio, λ, in a stationary curved duct flow so that they have the same dynamical meaning as those of the fully developed laminar flows. For the large values of Ro or λ, it is shown that the flow field satisfies the asymptotic invariance property, that is, there are strong quantitative similarities between the two flows such as flow patterns and friction factors for the same values of K(sub)TR and K(sub)TC.