• 대한기계학회논문집B
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• 제29권4호
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• pp.485-494
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• 2005

For the extensive investigation of local heat/mass transfer on the near-tip surface of turbine blade, experiments were conducted in a low speed stationary annular cascade. The turbine test section has a single stage composed of sixteen guide vanes and blades. The chord length and the height of the tested blade are 150 mm and about 125 mm, respectively. The blade has flat tip geometry and the mean tip clearance is about $2.5{\%}$ of the blade chord. Detailed mass transfer coefficient on the blade near-tip surface was obtained using a naphthalene sublimation technique. The inlet flow Reynolds number based on chord length and incoming flow velocity is changed from $1.0{\times}10^{5}\;to\;2.3{\times}10^{5}.$ Extremely complex heat transfer characteristics are observed on the blade surface due, to complicated flow patterns, such as flow acceleration, laminarization, transition, separation bubble and tip leakage flow. Especially, the suction side surface of the blade has higher heat/mass transfer coefficients and more complex distribution than the pressure side surface, which is related to the leakage flow. For all the tested Reynolds numbers, the heat/mass transfer characteristics on the turbine blade are the similar. The overall averaged $Sh_{c}$ values are proportional to $Re_{c}^{0.5}$ on the stagnation region and the laminar flow region such as the pressure side surface. However, since the flow is fully turbulent in the near-tip region, the heat/mass transfer coefficients are proportional to $Re_{c}^{0.8}.$

• Wind and Structures
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• 제35권1호
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• pp.1-20
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• 2022

This research work presents an experimental study's outcomes to reveal the impact of an O-ring on the flow control over a sphere placed in a turbulent boundary layer. The investigation is performed quantitatively and qualitatively using particle image velocimetry (PIV) and dye visualization. The sphere model having a diamater of 42.5 mm is located in a turbulent boundary layer flow over a smooth plate for gap ratios of 0≤G/D≤1.5 at Reynolds number of 5 × 10³. Flow characteristics, including patterns of instantaneous vorticity, streaklines, time-averaged streamlines, velocity vectors, velocity fluctuations, Reynolds stress correlations, and turbulence kinetic energy (), are compared and discussed for a naked sphere and spheres having O-rings. The boundary layer velocity gradient and proximity of the sphere to the flat plate profoundly influence the flow dynamics. At proximity ratios of G/D=0.1 and 0.25, a wall jet is formed between lower side of the sphere and flat plate, and velocity fluctuations increase in regions close to the wall. At G/D=0.25, the jet flow also induces local flow separations on the flat plate. At higher proximity ratios, the velocity gradient of the boundary layer causes asymmetries in the mean flow characteristics and turbulence values in the wake region. It is observed that the O-ring with various placement angles (𝜃) on the sphere has a considerable alteration in the flow structure and turbulence statistics on the wake. At lower placement angles, where the O-ring is closer to the forward stagnation point of the sphere, the flow control performance of the O-ring is limited; however, its impact on the flow separation becomes pronounced as it is moved away from the forward stagnation point. At G/D=1.50 for O-ring diameters of 4.7 (2 mm) and 7 (3 mm) percent of the sphere diameter, the -ring exhibits remarkable flow control at 𝜃=50° and 𝜃=55° before laminar flow separation occurrence on the sphere surface, respectively. This conclusion is yielded from narrowed wakes and reductions in turbulence statistics compared to the naked sphere model. The O-ring with a diameter of 3 mm and placement angle of 50° exhibits the most effective flow control. It decreases, in sequence, streamwise velocity fluctuations and length of wake recovery region by 45% and 40%, respectively, which can be evaluated as source of decrement in drag force.

• Korean Chemical Engineering Research
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• 제50권6호
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• pp.1034-1042
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• 2012

본 연구에서는 다양한 석탄 연구에 적용되고 있는 층류 반응기(LFR)를 이용하여 열분해와 연소 분위기에서 탄종에 따른 화염형상을 분석하였고, 휘발분 함량이 다른 두 석탄의 타르와 수트의 발생률을 구하였으며 이를 촤 입자의 표면적 및 표면 형상 변화와 함께 비교하였다. 본 연구에서 사용된 층류 반응기는 화염형상을 가시적으로 분석하기에 뛰어나므로 석탄이 반응할 때 생성되는 수트 클라우드를 측정하여 그 형상 변화를 근거로 탈휘발의 종료 지점을 가정하였다. 휘발분 함량이 많은 Berau 탄은 Glencore A.P. 탄보다 수트 클라우드의 폭과 길이가 증가하였고, 연소 분위기에서는 촤와 수트의 산화반응에 의하여 열분해 때보다 화염과 수트 클라우드의 길이가 짧아지면서 더 밝은 빛을 내었다. 포집높이 50 mm까지에서는 휘발분 함량이 많은 Berau 탄의 타르와 수트 발생률이 Glencore A.P. 탄보다 작았다. 이는 석탄 연료의 조성 중 Berau 탄내에 상대적으로 높은 산소 성분의 함량과 OH- 같은 라디칼들로 인해 타르가 산화되기 때문이다. 반면에, 50 mm 이후부터는 Berau 탄이 Glencore A.P. 탄보다 더 많은 타르와 수트의 발생률이 나타나며 탄종간에 수트 발생률의 역전현상이 일어나는데 이는 촤 입자 내부의 휘발물질과 탈휘발 과정에서 생성된 화염 속의 잔여 타르 및 light gas 성분이 반응하여 수트를 발생시켰기 때문이다. 이를 통해서 석탄 내의 휘발분의 함량과 산소농도는 수트 클라우드의 길이와 폭에 명확한 영향을 주며, 수트 발생률에 매우 중요한 인자라는 것을 확인할 수 있었다. SEM과 B.E.T.의 결과로부터 탈휘발이 종료된 후에도 촤 입자 내부의 잔존 휘발물들이 분출되면서 타르와 수트가 발생함을 확인할 수 있었고, 각 탄의 휘발분 함량과 기공의 발달 차이를 통해서 100 mm 이후에 나타난 타르와 수트의 발생률 역전 현상을 설명할 수 있었다.