Search Results - "Kwak, Jae Su"

Experimental optimization of a fan-shaped film cooling hole with 30 degrees-injection angle and 6-hole length-to-diameter ratio by Park, Sang Hyeon, Kang, Young Jun, Seo, Hyun Jae, Kwak, Jae Su, Kang, Young Seok

“…•The effect of the shape parameter of fan-shaped holes on film cooling effectiveness was experimentally investigated using the PSP (Pressure Sensitive Paint)…”
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Experimental Optimization of the Compound Angled Asymmetric Laidback Fan Shaped Film Cooling Hole by Jo, Ye Rim, Jeong, Jin Young, Kwak, Jae Su

“…In this study, the effect of shape variables on the film cooling effectiveness of the compound angled asymmetric laidback fan shaped hole was experimentally…”
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Effect of Mainstream Velocity on the Optimization of a Fan-Shaped Film-Cooling Hole on a Flat Plate by Lee, Soo In, Jung, Jin Young, Song, Yu Jin, Kwak, Jae Su

“…In this study, the effect of mainstream velocity on the optimization of a fan-shaped hole on a flat plate was experimentally investigated. The experiment was…”
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Effect of Mainstream Velocity on the Heat Transfer Coefficient of Gas Turbine Blade Tips by Jeong, Jin Young, Kim, Woojun, Kwak, Jae Su, Lee, Byung Ju, Chung, Jin Taek

“…This study experimentally investigated the effects of cascade inlet velocity on the distribution and the level of the heat transfer coefficient on a gas…”
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The Effects of Hole Arrangement and Density Ratio on the Heat Transfer Coefficient Augmentation of Fan-Shaped Film Cooling Holes by Kim, Young Seo, Jeong, Jin Young, Kwak, Jae Su, Chung, Heeyoon

“…An experimental study was performed to investigate the effects of the arrangement of fan-shaped film cooling holes and density ratio (DR) on heat transfer…”
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Large Eddy Simulations on Film Cooling Flow Behaviors with Upstream Turbulent Boundary Layer Generated by Circular Cylinder by Kang, Young Seok, Rhee, Dong-Ho, Song, Yu Jin, Kwak, Jae Su

“…Large eddy simulations on film cooling hole array on a flat plate was carried out to investigate upstream turbulence effect. Circular cylinders were configured…”
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Effects of turbine blade tip shape on total pressure loss and secondary flow of a linear turbine cascade by Nho, Young Cheol, Park, Jung Shin, Lee, Yong Jin, Kwak, Jae Su

“…► Effect of gas turbine blade tip shape on the tip leakage flow and total pressure loss. ► 11 tip shapes including plane, squealer, dimpled, and newly proposed…”
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Mass Flow Function Correlation for Solid and Honeycomb Land Labyrinth Seals including Fin Front Angle, Clearance, Fin Number and Honeycomb Geometry by Kim, Hyeok Je, Kang, Young Jun, Kim, Woojun, Jo, Ye Rim, Park, Suhyeon, Kwak, Jae Su

“…In this study, the effects of several geometry factors (fin front angle, clearance, number of fins, and honeycomb cell diameter and depth) on the mass flow…”
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Comparison of Aerodynamic Loss of a Gas Turbine Vane with Various Trailing Edge Cooling Schemes by Kim, Gi-Mun, Jeong, Jin-Young, Kang, Young-Jun, Kwak, Jae-Su

“…In this study, a comparison of aerodynamic loss of gas turbine vane with various trailing edge configurations was experimentally performed. For the trailing…”
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Heat transfer augmentation using a rib–dimple compound cooling technique by Choi, Eun Yeong, Choi, Yong Duck, Lee, Won Suk, Chung, Jin Teak, Kwak, Jae Su

“…Detailed distributions of the heat transfer coefficients in the channel with both angled ribs and dimples were measured using the transient liquid crystal…”
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Experimental Investigation on the Effects of DBD Plasma on the Film Cooling Effectiveness of a 30-Degree Slot by Kim, Ye, Kim, Gi, Shin, Youhwan, Kwak, Jae

“…The effects of dielectric barrier discharge (DBD) plasma on the film cooling effectiveness of a 30-degree slot was experimentally investigated in a low-speed…”
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Effects of rim location, rim height, and tip clearance on the tip and near tip region heat transfer of a gas turbine blade by Kwak, Jae Su, Ahn, Jaeyong, Han, Je-Chin

“…Effects of the rim height and the tip gap clearance on the heat transfer coefficients on the blade tip and near tip regions were measured with two different…”
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Development of a Plate-Fin Type Gas Turbine Recuperator by Kwak Jae-Su, Yang In-Young

“…A plate-fin type recuperator for a gas turbine/fuel cell hybrid power generation system was designed, manufactured, and tested. Performance analysis shows that…”
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Numerical and experimental studies on the mixing characteristics of two jets with inclined angles in a rectangular chamber by Han, Doo-Hee, Shin, Jun-Su, Kang, Jeong-Seok, Park, Jung-Shin, Park, Sun-Sang, Kwak, Jae-Su, Sung, Hong-Gye, Choi, Ho-Jin

“…Mixing characteristics in a rectangular chamber are investigated using experimental and numerical methods. A mixing chamber with an axial inlet (representing…”
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Uncertainty Analysis and ANOVA for the Measurement Reliability Estimation of Altitude Engine Test by Lee, Jin-Kun, Yang, In-Young, Yang, Soo-Seok, Kwak, Jae-Su

“…The altitude engine test is carried out to measure the performance of the engine of flight vehicle at the high altitude environment prior to the flight test…”
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Effect of hole shape on the heat transfer in a rectangular duct with perforated blockage walls by Shin, Somin, Kwak, Jae Su

“…Heat transfer coefficients were measured by the improved hue detection based liquid crystal technique in a turbine blade internal cooling passage model with…”
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Development of a Plate-Fin Type Gas Turbine Recuperator by Kwak, Jae Su, Yang, Inyoung

“…A plate-fin type recuperator for a gas turbine/fuel cell hybrid power generation system was designed, manufactured, and tested. Performance analysis shows that…”
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Effects of trench configuration on the film cooling effectiveness of a fan-shaped hole by Song, Yu Jin, Park, Sang Hyeon, Kang, Young Jun, Kwak, Jae Su

“…•Study on the film cooling effectiveness of a fan-shaped hole with various trench configurations was conducted.•The effect of flow conditions such as density…”
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Uncertainty Analysis and ANOVA for the Measurement Reliability Estimation of Altitude Engine Test by LEE, Jinkun, YANG, Inyoung, YANG, Sooseok, JAE SU KWAK

“…The altitude engine test is carried out to measure the performance of the engine of flight vehicle at the high altitude environment prior to the flight test…”
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Experimental study on heat transfer characteristics in a ribbed channel with dimples, semi-spherical protrusions, or oval protrusions by Jang, Han Na, Park, Jung Shin, Kwak, Jae Su

“…•Study on the heat transfer augmentation of a ribbed channel using dimple or protrusion.•Detailed distribution of the heat transfer coefficient was obtained…”
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